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 63097U 26145.45104829 +.00000000 +00000-0 -35047-4 0 00003
2 63097 70.0003 160.7735 0004449 267.2109 92.8541 14.98330546 06
| Epoch (UTC): | 25 May 2026 10:49:30 |
| Eccentricity: | 0.0004449 |
| inclination: | 70.0003° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.7735° |
| argument of perigee: | 267.2109° |
| revolutions per day: | 14.98330546 |
| mean anomaly at epoch: | 92.8541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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