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UND ROADS 2

In orbit NORAD 64549 BZMH-1691-0385-6822-7921 United States of America

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

179

Observations all time

Mission information
Spacecraft name
UND ROADS 2
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2025-06-23 21:25:00
Separation time
2025-06-23 22:22:26
Last observers
Observer
Time of receipt
2026-03-02 12:23:49 UTC
2025-07-15 13:51:58 UTC
2025-07-11 21:05:57 UTC
2025-07-10 10:29:57 UTC
2025-07-06 00:09:30 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
485.79 km
Apogee
489.39 km
Inclination
97.5°
Period
94.4 min
Semi-major axis
6865.6 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 13:08:41 UTC
Two-line elements (TLE)
1 64549U 25135X   26285.28273904  .00006780  00000-0  27396-3 0  9993
2 64549 97.4901 41.3153 0002582 73.6810 286.4712 15.25078240 72754
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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
2026-10-14 00:08:04 ROADS 2
NORAD 64549
YAOGAN-1 DEB
NORAD 36365
4.398 5.16 2.2e-07
2026-10-14 07:40:20 HXMT (HUIYAN)
NORAD 42758
ROADS 2
NORAD 64549
3.882 14.25 1.4e-07
2026-10-14 18:59:39 TIANMU-1 17
NORAD 58702
ROADS 2
NORAD 64549
4.087 8.66 2.2e-07
2026-10-15 05:42:19 YAOGAN-36 05A
NORAD 57452
ROADS 2
NORAD 64549
4.067 8.19 2.3e-07
2026-10-15 08:04:04 YAOGAN-36 05A
NORAD 57452
ROADS 2
NORAD 64549
2.427 8.20 6.5e-07
2026-10-15 09:31:16 ROADS 2
NORAD 64549
HULIANWANG JISHU SHIYAN 9D
NORAD 68834
4.891 14.77 7.5e-08
2026-10-18 17:30:45 ROADS 2
NORAD 64549
CZ-4B DEB
NORAD 35573
4.667 0.68 2.0e-07

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