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Oasis Alpha

In orbit NORAD 69936 DJQF-3933-8140-4498-1525

Time in UTC

21:23

Next pass · Обозерский

—

No observations scheduled

7

Observations over 30 days

0%

Successful observations

0

Frames received

Mission information
Spacecraft name
Oasis Alpha
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
2026-07-07 07:12:00
Separation time
2026-07-07 08:10:42
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
580.11 km
Apogee
593.11 km
Inclination
97.7°
Period
96.5 min
Semi-major axis
6964.7 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:21 UTC
Two-line elements (TLE)
1 69936U 26156BV  26282.66762522  .00001511  00000-0  15192-3 0  9998
2 69936 97.7379 181.5753 0009330 191.9349 168.1651 14.92676855 14071
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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 06:09:37 OASIS ALPHA
NORAD 69936
PSLV DEB
NORAD 27089
3.884 13.46 1.6e-07
2026-10-12 15:12:13 TRANSPORTER-17 OBJECT J
NORAD 69877
OASIS ALPHA
NORAD 69936
4.604 0.01 2.1e-07
2026-10-12 16:27:33 OASIS ALPHA
NORAD 69936
NOAA 17 DEB
NORAD 48165
4.548 14.98 7.7e-08
2026-10-14 04:12:30 JACK K
NORAD 66659
OASIS ALPHA
NORAD 69936
3.381 3.75 3.8e-07
2026-10-14 07:29:21 OASIS ALPHA
NORAD 69936
COROT
NORAD 29678
3.012 14.57 2.1e-07
2026-10-14 19:08:36 IRIDE-MS2-HEO-1
NORAD 62697
OASIS ALPHA
NORAD 69936
1.723 15.00 5.3e-07
2026-10-14 23:31:24 YAM-16
NORAD 68992
OASIS ALPHA
NORAD 69936
4.548 0.49 2.1e-07
2026-10-15 11:32:29 COSMOS 2523
NORAD 42986
OASIS ALPHA
NORAD 69936
4.603 12.20 1.4e-07
2026-10-15 20:26:16 NULINK-1
NORAD 69002
OASIS ALPHA
NORAD 69936
4.329 0.45 2.4e-07
2026-10-15 21:45:54 OASIS ALPHA
NORAD 69936
CZ-6A DEB
NORAD 55902
2.016 14.94 4.0e-07
2026-10-15 22:02:47 NULINK-1
NORAD 69002
OASIS ALPHA
NORAD 69936
2.399 0.45 7.7e-07
2026-10-16 03:40:35 NULINK-1
NORAD 69002
OASIS ALPHA
NORAD 69936
4.941 0.45 1.8e-07
2026-10-16 05:17:06 NULINK-1
NORAD 69002
OASIS ALPHA
NORAD 69936
2.794 0.45 5.7e-07
2026-10-16 06:06:30 MISR-D 1
NORAD 69908
OASIS ALPHA
NORAD 69936
4.196 0.01 2.5e-07
2026-10-16 08:57:00 ICEYE-X42
NORAD 62698
OASIS ALPHA
NORAD 69936
4.671 14.98 7.2e-08
2026-10-16 10:08:15 OASIS ALPHA
NORAD 69936
FENGYUN 1C DEB
NORAD 32409
1.818 3.98 1.3e-06
2026-10-16 10:33:33 ICEYE-X42
NORAD 62698
OASIS ALPHA
NORAD 69936
3.597 14.98 1.2e-07
2026-10-16 12:10:06 ICEYE-X42
NORAD 62698
OASIS ALPHA
NORAD 69936
4.889 14.98 6.6e-08
2026-10-16 16:38:56 ANDURIL-216
NORAD 69879
OASIS ALPHA
NORAD 69936
4.831 0.01 1.9e-07
2026-10-16 17:23:10 ANDURIL-216
NORAD 69879
OASIS ALPHA
NORAD 69936
3.980 0.01 2.7e-07
2026-10-16 18:09:15 GRUS-3C
NORAD 69891
OASIS ALPHA
NORAD 69936
4.817 0.02 1.9e-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