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 63038U 26145.62000682 +.00000000 +00000-0 +24479-3 0 00004
2 63038 53.1577 260.8972 0001164 90.5320 269.5814 15.30183582 06
| Epoch (UTC): | 25 May 2026 14:52:48 |
| Eccentricity: | 0.0001164 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 260.8972° |
| argument of perigee: | 90.5320° |
| revolutions per day: | 15.30183582 |
| mean anomaly at epoch: | 269.5814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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