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TeLEOS-2

In orbit NORAD 56310 KIVN-1503-3648-0138-3978 Singapore

2023

Launch

0

Observations all time

Mission information
Spacecraft name
TeLEOS-2
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
2023-04-22 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
583.50 km
Apogee
584.58 km
Inclination
10.0°
Period
96.2 min
Semi-major axis
6962.2 km
Velocity
7.58 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:48 UTC
Two-line elements (TLE)
1 56310U 23057C   26283.06281037  .00005615  00000-0  42275-3 0  9990
2 56310 9.9870 87.7374 0000772 268.6722 91.3403 14.96413840190038
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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 04:20:04 STARLINK-5510
NORAD 55647
TELEOS-2
NORAD 56310
0.529 8.51 4.0e-04
2026-10-11 05:08:06 STARLINK-5510
NORAD 55647
TELEOS-2
NORAD 56310
0.657 8.51 2.6e-04
2026-10-11 06:21:53 STARLINK-3088
NORAD 49163
TELEOS-2
NORAD 56310
4.130 7.61 6.9e-06
2026-10-11 07:54:38 STARLINK-5928
NORAD 55958
TELEOS-2
NORAD 56310
2.047 7.58 2.8e-05
2026-10-11 08:42:40 STARLINK-5928
NORAD 55958
TELEOS-2
NORAD 56310
3.756 7.58 8.3e-06
2026-10-11 12:17:46 TELEOS-2
NORAD 56310
STARLINK-36211
NORAD 67218
2.486 8.67 1.8e-05
2026-10-11 13:05:47 TELEOS-2
NORAD 56310
STARLINK-36211
NORAD 67218
2.447 8.67 1.9e-05
2026-10-11 13:53:08 TELEOS-2
NORAD 56310
STARLINK-6029
NORAD 56803
2.978 8.60 1.3e-05
2026-10-12 12:38:04 TELEOS-2
NORAD 56310
PE2_FLT1 (TYVAK-0261)
NORAD 59105
4.698 10.54 1.5e-07
2026-10-13 10:33:04 TELEOS-2
NORAD 56310
STARLINK-34604
NORAD 64801
3.862 9.21 7.3e-06
2026-10-14 05:36:49 STARLINK-3089
NORAD 49166
TELEOS-2
NORAD 56310
4.928 7.71 4.8e-06
2026-10-14 07:59:37 TELEOS-2
NORAD 56310
STARLINK-36172
NORAD 67020
2.214 9.64 2.2e-05
2026-10-14 14:23:51 TELEOS-2
NORAD 56310
STARLINK-35913
NORAD 67004
1.653 9.63 3.9e-05
2026-10-14 14:26:29 SMDC ONE 2.4
NORAD 39469
TELEOS-2
NORAD 56310
4.979 12.58 1.1e-07
2026-10-14 21:28:24 STARLINK-5283
NORAD 55396
TELEOS-2
NORAD 56310
3.793 9.74 7.4e-06
2026-10-15 06:36:17 TELEOS-2
NORAD 56310
ATLAS 28E DEB
NORAD 20575
3.305 11.00 2.9e-07
2026-10-15 17:15:46 TELEOS-2
NORAD 56310
LEMUR-2-BALTO
NORAD 63395
3.452 11.98 2.5e-07
2026-10-15 21:16:29 TELEOS-2
NORAD 56310
STARLINK-36193
NORAD 67099
2.327 9.44 2.0e-05
2026-10-16 01:32:47 APRIZESAT 7
NORAD 39416
TELEOS-2
NORAD 56310
3.484 12.22 2.4e-07
2026-10-16 01:35:19 STARLINK-5929
NORAD 55959
TELEOS-2
NORAD 56310
0.844 7.69 1.6e-04
2026-10-16 02:23:21 STARLINK-5929
NORAD 55959
TELEOS-2
NORAD 56310
1.869 7.69 3.4e-05
2026-10-16 04:28:45 TELEOS-2
NORAD 56310
STARLINK-35864
NORAD 67081
1.238 9.46 7.0e-05
2026-10-16 21:09:39 TELEOS-2
NORAD 56310
STARLINK-6031
NORAD 56810
1.762 9.06 3.6e-05
2026-10-16 21:57:40 TELEOS-2
NORAD 56310
STARLINK-6031
NORAD 56810
4.413 9.06 5.7e-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