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 63380U 26145.46137892 +.00000000 +00000-0 +35998-3 0 00008
2 63380 53.1599 55.8556 0001380 94.3579 265.7579 15.30207721 06
| Epoch (UTC): | 25 May 2026 11:04:23 |
| Eccentricity: | 0.0001380 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 55.8556° |
| argument of perigee: | 94.3579° |
| revolutions per day: | 15.30207721 |
| mean anomaly at epoch: | 265.7579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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