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 62931U 26145.12331093 +.00000000 +00000-0 +17729-3 0 00003
2 62931 97.8966 197.2475 0001162 113.4952 246.6381 14.76935524 04
| Epoch (UTC): | 25 May 2026 02:57:34 |
| Eccentricity: | 0.0001162 |
| inclination: | 97.8966° |
| perigee height: | 638 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 197.2475° |
| argument of perigee: | 113.4952° |
| revolutions per day: | 14.76935524 |
| mean anomaly at epoch: | 246.6381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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