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 48881U 26145.59903670 +.00000000 +00000-0 -15732-4 0 00002
2 48881 97.6585 271.0993 0000991 110.1434 249.9897 15.01258155 06
| Epoch (UTC): | 25 May 2026 14:22:36 |
| Eccentricity: | 0.0000991 |
| inclination: | 97.6585° |
| perigee height: | 562 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 271.0993° |
| argument of perigee: | 110.1434° |
| revolutions per day: | 15.01258155 |
| mean anomaly at epoch: | 249.9897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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