Issue 140

Update: TJS-3 & TJS-10 To the Merge

5 Mar 2026: As noted in the last edition of the Flash , Chinese space operators maneuvered both TJS-10 (58204) and TJS-3 (43874) in early February resulting in the two satellites heading toward one another. TJS-10 (58204) remains above the GEO belt and maintains a 1.9°/day westward drift. For its part, TJS-3 increased…

5 Mar 2026: As noted in the last edition of the Flash, Chinese space operators maneuvered both TJS-10 (58204) and TJS-3 (43874) in early February resulting in the two satellites heading toward one another. TJS-10 (58204) remains above the GEO belt and maintains a 1.9°/day westward drift. For its part, TJS-3 increased its SMA 81km on 27 Feb, slowing its eastward drift from ~1.3°/day to 0.2°/day. In their current orbits (as of 5 Mar) TJS-10 and TJS-3 are on course to have a point of closest approach on 20 Mar 2026 at ~1630Z over ~90.4°E longitude.

Recall that TJS-3 and TJS-10 operated in vicinity of one another during TJS-10’s first year on orbit from Nov 2023 – Nov 2024. It appears China purposefully launched TJS-10 into a co-planar orbit with TJS-3 (TJS-3 also conducted minor plane change maneuvers prior to TJS-10 launch). Comparing their current orbital parameters TJS-10 and TJS-3 remain nearly co-planar. Their inclination values are separated by only 0.001° and RAAN by 0.019°.

TJS-3’s most recent maneuver not only slowed its eastward drift, but also changed TJS-3’s eccentricity (orbit shape) to more closely match that of TJS-10. Prior to the maneuver TJS-3’s orbit had an eccentricity of 0.00006; post maneuver the eccentricity was 0.00169. TJS-10’s eccentricity is 0.00111. China has not aligned the Argument of Perigee for the two satellites, TJS-3 Arg of Perigee is 345.1° and TJS-10 is 234.0°. Looking at the two satellites at point of closest approach (assumes no further maneuvers) TJS-3 and TJS-10 will be separated by <1km in cross-track and in-track and just under 200km in radial-track.

Given the past history of these two satellites I anticipate TJS-10 will decrease its SMA prior to crossing paths with TJS-3 and position itself just to the east of TJS-3. In 2024 this distance ranged from 60-200km. We will be able to observe future maneuvers from both satellites…stay tuned!




1 Feb – 5 Mar Orbital History of TJS-10 (Left) and TJS-3 (Right)
TJS-10 Holding Steady after 3-4 Feb SMA Increase
TJS-3 Increased SMA 81km 27 Feb 2026 Remains 21km Below GEO
(celestrak.org)


5 Mar: TJS-3 and TJS-10 Current Positions and Point Of Closest Approach Projection
(saberastro.com)


Note Radial Distance Primary Source of Separation

Projected Point of Closest Approach 20 Mar 2026
Note Radial Distance Primary Source of Separation
(saberastro.com)