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PROSPERO

In orbit NORAD 5580 MDNJ-2178-8370-7421-2425 United Kingdom

Time in UTC

21:07

Next pass · Обозерский

—

No observations scheduled

21

Observations over 30 days

2%

Successful observations

8

Frames, latest 2026-09-16 16:28 UTC

British Satellite

Mission description
Mission information
Spacecraft name
PROSPERO
Other names
BLACK ARROW
X-3
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
Separation time
Last observers
Observer
Time of receipt
2026-09-16 16:28:42 UTC
2026-09-16 02:50:29 UTC
2026-09-15 23:27:18 UTC
2026-09-15 20:03:22 UTC
2026-09-15 19:54:04 UTC
Satellite appearance

Credit: Geni CC BY-SA 4.0 source

Data for the last 30 days
Orbital parameters of the satellite
Perigee
522.15 km
Apogee
1246.65 km
Inclination
82.0°
Period
102.7 min
Semi-major axis
7262.5 km
Velocity
7.35 km/s
Orbital elements
TLE source
Space-Track.org
TLE updated
2026-10-08 08:46:42 UTC
Two-line elements (TLE)
1 05580U 71093A   26280.72142158  .00000524  00000-0  11046-3 0  9992
2 05580 82.0413 192.0386 0498790 264.4191 89.9917 14.01888260764290
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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 04:49:34 UMBRA-09
NORAD 60541
PROSPERO (BLACK ARROW)
NORAD 5580
3.022 15.33 1.6e-07
2026-10-12 19:25:25 ONEWEB-0177
NORAD 48074
PROSPERO (BLACK ARROW)
NORAD 5580
4.452 11.65 4.6e-07
2026-10-12 20:15:19 FSI-SAT2
NORAD 68792
PROSPERO (BLACK ARROW)
NORAD 5580
3.551 12.97 2.1e-07
2026-10-13 00:33:46 ONEWEB-0307
NORAD 49189
PROSPERO (BLACK ARROW)
NORAD 5580
1.649 11.66 3.4e-06
2026-10-13 10:50:28 ONEWEB-0355
NORAD 49218
PROSPERO (BLACK ARROW)
NORAD 5580
3.838 11.69 6.2e-07
2026-10-13 15:05:44 OBJECT F
NORAD 100614
PROSPERO (BLACK ARROW)
NORAD 5580
2.233 15.27 3.0e-07
2026-10-14 18:30:41 OBJECT A
NORAD 100609
PROSPERO (BLACK ARROW)
NORAD 5580
2.500 15.25 2.4e-07
2026-10-15 13:17:19 OBJECT B
NORAD 69098
PROSPERO (BLACK ARROW)
NORAD 5580
3.661 15.31 1.1e-07
2026-10-16 07:52:57 FIREFLY-2
NORAD 62704
PROSPERO (BLACK ARROW)
NORAD 5580
2.812 15.28 1.9e-07
2026-10-17 01:17:51 OBJECT N
NORAD 100967
PROSPERO (BLACK ARROW)
NORAD 5580
1.644 14.98 6.2e-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