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R5-S2-2.0

In orbit NORAD 60207 IITE-3822-1649-0687-2055

2024

Launch

0

Observations all time

Mission information
Spacecraft name
R5-S2-2.0
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2024-07-04 04:04:00
Separation time
2024-07-04 04:54:23
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
408.36 km
Apogee
428.47 km
Inclination
97.2°
Period
93.0 min
Semi-major axis
6796.5 km
Velocity
7.66 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:49 UTC
Two-line elements (TLE)
1 60207U 24125E   26283.27429450  .00020613  00000-0  38900-3 0  9998
2 60207 97.2203 134.9824 0014795 162.0841 198.0935 15.48369772126971
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-11 06:01:39 R5-S2
NORAD 60207
CREW DRAGON 13
NORAD 100882
3.545 8.25 3.0e-07
2026-10-11 06:01:39 R5-S2
NORAD 60207
CYGNUS NG-24
NORAD 68689
3.545 8.25 3.0e-07
2026-10-11 06:01:39 R5-S2
NORAD 60207
PROGRESS-MS 34
NORAD 68837
3.545 8.25 3.0e-07
2026-10-11 06:01:39 R5-S2
NORAD 60207
SOYUZ-MS 29
NORAD 100057
3.545 8.25 3.0e-07
2026-10-11 06:01:39 R5-S2
NORAD 60207
PROGRESS-MS 35
NORAD 100712
3.545 8.25 3.0e-07
2026-10-11 06:01:39 POISK
NORAD 36086
R5-S2
NORAD 60207
3.638 8.25 2.9e-07
2026-10-11 06:01:39 ISS (DESTINY)
NORAD 26700
R5-S2
NORAD 60207
3.638 8.25 2.8e-06
2026-10-11 06:01:39 ISS (NAUKA)
NORAD 49044
R5-S2
NORAD 60207
3.638 8.25 2.9e-07
2026-10-11 06:01:39 ISS (ZARYA)
NORAD 25544
R5-S2
NORAD 60207
3.638 8.25 1.7e-05
2026-10-11 06:01:39 ISS (UNITY)
NORAD 25575
R5-S2
NORAD 60207
3.638 8.25 3.7e-06
2026-10-11 06:01:39 ISS (ZVEZDA)
NORAD 26400
R5-S2
NORAD 60207
3.638 8.25 2.2e-05
2026-10-11 13:41:40 STARLINK-1413
NORAD 45689
R5-S2
NORAD 60207
1.048 6.19 1.1e-04
2026-10-13 03:13:58 ION SCV-006
NORAD 52761
R5-S2
NORAD 60207
4.489 7.26 2.0e-07
2026-10-13 03:34:18 STARLINK-1153
NORAD 45080
R5-S2
NORAD 60207
3.146 14.82 5.6e-06
2026-10-15 03:49:29 STARLINK-1553
NORAD 46348
R5-S2
NORAD 60207
4.631 14.48 2.8e-06
2026-10-16 21:22:51 R5-S2
NORAD 60207
STARLINK-38421
NORAD 100631
3.806 4.65 8.8e-06

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite