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DISCO-2

In orbit NORAD 68431 HWUY-3165-6126-0472-2513 Denmark

Time in UTC

08:12

Next pass · Баган

15.10 11:21

Scheduled · Геоскан

55

Observations over 30 days

61%

Successful observations

500

Frames, latest 2026-10-15 02:09 UTC

Mission information
Spacecraft name
DISCO-2
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-03-29 00:00:00
Separation time
Last observers
Observer
Time of receipt
2026-10-15 02:09:37 UTC
2026-10-15 00:37:33 UTC
2026-10-12 10:49:10 UTC
2026-10-11 01:49:14 UTC
2026-09-28 01:15:25 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
500.06 km
Apogee
501.59 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6879.0 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68431U 26067R   26287.15019177  .00009330  00000-0  42791-3 0  9990
2 68431 97.4760 244.4823 0001109 15.5456 344.5814 15.20656866 30019
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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
2026-10-15 09:57:18 IRIDE-MS1-EAGLET 2-7
NORAD 66701
DISCO-2
NORAD 68431
1.315 12.69 1.6e-06
2026-10-15 15:17:41 TOMORROW-S9
NORAD 66309
DISCO-2
NORAD 68431
4.728 8.62 1.7e-07
2026-10-15 21:01:29 SNUSAT-2
NORAD 43782
DISCO-2
NORAD 68431
4.481 11.06 1.6e-07
2026-10-16 12:00:39 ALSAT-3A
NORAD 67474
DISCO-2
NORAD 68431
3.890 12.75 1.8e-07
2026-10-16 17:35:07 DISCO-2
NORAD 68431
HAWK-14C
NORAD 68441
4.894 0.08 1.8e-07
2026-10-16 18:19:47 TRANSPORTER-15 OBJECT AA
NORAD 66690
DISCO-2
NORAD 68431
3.669 12.62 2.0e-07
2026-10-17 01:26:16 DISCO-2
NORAD 68431
TRANSPORTER-18 OBJECT BP
NORAD 100944
4.215 12.51 1.6e-07
2026-10-17 18:48:33 DISCO-2
NORAD 68431
TRANSPORTER-18 OBJECT BB
NORAD 100932
4.349 12.51 1.5e-07
2026-10-18 06:27:01 YAOGAN-39 02C
NORAD 57890
DISCO-2
NORAD 68431
4.837 10.33 1.4e-07
2026-10-18 07:26:34 DISCO-2
NORAD 68431
TRANSPORTER-18 OBJECT BQ
NORAD 100945
3.445 12.51 2.4e-07
2026-10-18 10:54:05 DISCO-2
NORAD 68431
COSMOS 2251 DEB
NORAD 36441
4.943 15.18 6.2e-08
2026-10-18 12:59:55 DISCO-2
NORAD 68431
ION SCV-019 (ASTOUNDING ALEXANDRA)
NORAD 68435
3.577 0.02 3.4e-07
2026-10-18 14:35:41 DISCO-2
NORAD 68431
ION SCV-019 (ASTOUNDING ALEXANDRA)
NORAD 68435
4.946 0.02 1.8e-07
2026-10-18 16:55:05 DISCO-2
NORAD 68431
TRANSPORTER-18 OBJECT BX
NORAD 100952
4.266 12.51 1.5e-07
2026-10-18 16:57:38 DISCO-2
NORAD 68431
ION SCV-019 (ASTOUNDING ALEXANDRA)
NORAD 68435
4.644 0.02 2.0e-07
2026-10-18 21:28:43 STARLINK-5927
NORAD 55934
DISCO-2
NORAD 68431
3.002 15.08 5.3e-06
2026-10-19 00:49:21 CARTOSAT-2C
NORAD 41599
DISCO-2
NORAD 68431
1.666 11.64 1.1e-06
2026-10-19 04:17:54 YAOGAN-39 05C
NORAD 58559
DISCO-2
NORAD 68431
4.804 13.35 1.1e-07
2026-10-21 01:56:30 DISCO-2
NORAD 68431
SL-16 DEB
NORAD 39708
0.429 7.11 2.2e-05

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