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NUSHSat1

In orbit NORAD 63211 AGMX-2508-1337-4945-9939 Singapore

Time in UTC

17:58

Next pass · Мурманск

—

No observations scheduled

1

Observations over 30 days

92%

Successful observations

9k

Frames, latest 2026-10-09 21:46 UTC

Mission information
Spacecraft name
NUSHSat1
Frequency usage status
Violator
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9
Spaceport
База Вандерберг
Launch time
2025-03-15 06:43:00
Separation time
Last observers
Observer
Time of receipt
2026-02-09 21:30:12 UTC
2025-07-02 21:38:24 UTC
2025-06-12 10:19:33 UTC
2025-06-12 08:48:18 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
439.36 km
Apogee
445.78 km
Inclination
97.4°
Period
93.5 min
Semi-major axis
6820.7 km
Velocity
7.63 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-09 12:46:41 UTC
Two-line elements (TLE)
1 63211U 25052B   26282.17176202  .00021379  00000-0  53411-3 0  9992
2 63211 97.3824 180.2815 0004707 63.5105 296.6624 15.40162228 87664
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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 05:47:34 NUSHSAT1
NORAD 63211
COSMOS 2251 DEB
NORAD 33821
2.174 4.98 8.9e-07
2026-10-11 17:49:16 THEA
NORAD 43796
NUSHSAT1
NORAD 63211
4.833 15.11 6.8e-08
2026-10-11 19:22:52 THEA
NORAD 43796
NUSHSAT1
NORAD 63211
4.931 15.11 6.5e-08
2026-10-12 10:35:57 NUSHSAT1
NORAD 63211
ARIANE 40 R/B
NORAD 25979
4.219 14.73 1.4e-06
2026-10-12 20:17:52 NUSHSAT1
NORAD 63211
NAOS
NORAD 65317
2.438 15.14 2.6e-07
2026-10-13 02:50:28 NUSHSAT1
NORAD 63211
CZ-6A DEB
NORAD 60774
4.023 11.65 1.9e-07
2026-10-13 23:34:12 OBJECT V
NORAD 57185
NUSHSAT1
NORAD 63211
4.440 15.16 8.0e-08
2026-10-15 16:59:03 CS2
NORAD 49262
NUSHSAT1
NORAD 63211
4.455 15.06 8.2e-08
2026-10-15 18:48:38 GREGOIRE
NORAD 56946
NUSHSAT1
NORAD 63211
3.635 12.34 2.2e-07
2026-10-17 00:30:53 NUSHSAT1
NORAD 63211
OBJECT H
NORAD 51953
0.600 14.06 6.1e-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