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 48487U 26145.55987227 +.00000000 +00000-0 +17023-4 0 00004
2 48487 53.1577 196.5073 0001061 90.1704 269.9419 15.31707104 00
| Epoch (UTC): | 25 May 2026 13:26:12 |
| Eccentricity: | 0.0001061 |
| inclination: | 53.1577° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 196.5073° |
| argument of perigee: | 90.1704° |
| revolutions per day: | 15.31707104 |
| mean anomaly at epoch: | 269.9419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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