RU | EN | ZH --:-- UTC Sign in

Black Kite-1

In orbit NORAD 66683 BMYD-8328-6159-7072-4807 Taiwan

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
Black Kite-1
Other names
8U RIoT-1
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
2025-11-28 18:44:30
Separation time
2025-11-28 19:39:30
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
493.70 km
Apogee
499.67 km
Inclination
97.4°
Period
94.6 min
Semi-major axis
6874.8 km
Velocity
7.61 km/s
Orbital elements
TLE source
Space-Track.org
TLE updated
2026-10-08 08:46:45 UTC
Two-line elements (TLE)
1 66741U 25276CD  26280.91419984  .00005025  00000-0  22293-3 0  9992
2 66741 97.4151 353.0126 0004344 328.4407 31.6568 15.22028263 44868
Copy content
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 08:52:59 6GSTARLAB
NORAD 66683
DB SKYFORGE CORE TU
NORAD 68445
4.795 12.70 1.2e-07
2026-10-11 09:57:00 6GSTARLAB
NORAD 66683
CAS500-2
NORAD 69013
3.895 15.07 1.0e-07
2026-10-11 22:35:44 6GSTARLAB
NORAD 66683
JEN-1
NORAD 69006
4.307 15.07 8.5e-08
2026-10-12 00:10:32 6GSTARLAB
NORAD 66683
JEN-1
NORAD 69006
3.696 15.07 1.2e-07
2026-10-12 01:45:28 6GSTARLAB
NORAD 66683
HELIOS
NORAD 69021
4.719 15.08 7.1e-08
2026-10-12 12:29:49 TIANYI B
NORAD 64049
6GSTARLAB
NORAD 66683
1.862 0.26 1.3e-06
2026-10-12 18:44:01 PREFIRE-2
NORAD 59881
6GSTARLAB
NORAD 66683
3.909 14.28 1.3e-07
2026-10-12 21:59:17 OBJECT E
NORAD 61231
6GSTARLAB
NORAD 66683
3.962 0.17 2.8e-07
2026-10-12 22:01:28 STRIX-3
NORAD 59224
6GSTARLAB
NORAD 66683
4.856 10.97 1.4e-07
2026-10-12 23:34:10 OBJECT E
NORAD 61231
6GSTARLAB
NORAD 66683
4.718 0.17 2.0e-07
2026-10-13 00:21:35 OBJECT E
NORAD 61231
6GSTARLAB
NORAD 66683
4.321 0.17 2.4e-07
2026-10-13 01:08:44 LEGION 2
NORAD 59626
6GSTARLAB
NORAD 66683
0.702 0.72 9.0e-06
2026-10-13 03:03:00 6GSTARLAB
NORAD 66683
BRO-21
NORAD 69007
1.109 15.07 1.3e-06
2026-10-13 03:20:53 STARLINK-2722
NORAD 48472
6GSTARLAB
NORAD 66683
3.029 9.77 1.2e-05
2026-10-13 03:41:05 6GSTARLAB
NORAD 66683
COSMOS 2251 DEB
NORAD 34449
1.243 15.09 1.0e-06
2026-10-13 14:36:51 6GSTARLAB
NORAD 66683
HAWK-13C
NORAD 67393
4.869 9.01 1.5e-07
2026-10-13 15:42:11 6GSTARLAB
NORAD 66683
BALKAN-2
NORAD 69024
3.704 15.08 1.1e-07
2026-10-13 16:59:10 6GSTARLAB
NORAD 66683
HAWK-13A
NORAD 67392
4.377 9.06 1.9e-07
2026-10-14 02:44:57 STARLINK-4478
NORAD 53529
6GSTARLAB
NORAD 66683
3.502 14.62 4.6e-06
2026-10-14 13:34:55 6GSTARLAB
NORAD 66683
COSMOS 2251 DEB
NORAD 36551
4.251 11.71 1.7e-07
2026-10-15 15:07:23 6GSTARLAB
NORAD 66683
JACKAL-004
NORAD 69012
4.363 15.07 8.3e-08
2026-10-15 15:37:38 QB50P2
NORAD 40032
6GSTARLAB
NORAD 66683
2.950 8.28 4.4e-07
2026-10-17 00:51:18 6GSTARLAB
NORAD 66683
DB CHARMS ND
NORAD 68455
3.088 12.69 2.9e-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