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 63221U 26145.45544262 +.00000000 +00000-0 +16059-3 0 00001
2 63221 97.3917 38.0083 0002553 189.8152 170.3034 15.21737172 07
| Epoch (UTC): | 25 May 2026 10:55:50 |
| Eccentricity: | 0.0002553 |
| inclination: | 97.3917° |
| perigee height: | 499 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 38.0083° |
| argument of perigee: | 189.8152° |
| revolutions per day: | 15.21737172 |
| mean anomaly at epoch: | 170.3034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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