View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65837U 26145.54303201 +.00000000 +00000-0 +69621-3 0 00005
2 65837 53.1581 91.1080 0001134 87.6725 272.4407 15.34400100 01
| Epoch (UTC): | 25 May 2026 13:01:57 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 91.1080° |
| argument of perigee: | 87.6725° |
| revolutions per day: | 15.34400100 |
| mean anomaly at epoch: | 272.4407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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