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 63220U 26145.64344260 +.00000000 +00000-0 +23605-3 0 00002
2 63220 97.3995 39.4134 0003726 175.8803 184.2466 15.24155721 05
| Epoch (UTC): | 25 May 2026 15:26:33 |
| Eccentricity: | 0.0003726 |
| inclination: | 97.3995° |
| perigee height: | 491 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 39.4134° |
| argument of perigee: | 175.8803° |
| revolutions per day: | 15.24155721 |
| mean anomaly at epoch: | 184.2466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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