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 62701U 26145.63791345 +.00000000 +00000-0 +13730-3 0 00002
2 62701 97.7070 224.2365 0005211 53.1337 307.0359 14.92799367 07
| Epoch (UTC): | 25 May 2026 15:18:35 |
| Eccentricity: | 0.0005211 |
| inclination: | 97.7070° |
| perigee height: | 586 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 224.2365° |
| argument of perigee: | 53.1337° |
| revolutions per day: | 14.92799367 |
| mean anomaly at epoch: | 307.0359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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