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 62625U 26145.14879689 +.00000000 +00000-0 +39757-3 0 00008
2 62625 97.4020 227.1104 0004965 52.7896 307.3796 15.28634230 02
| Epoch (UTC): | 25 May 2026 03:34:16 |
| Eccentricity: | 0.0004965 |
| inclination: | 97.4020° |
| perigee height: | 476 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 227.1104° |
| argument of perigee: | 52.7896° |
| revolutions per day: | 15.28634230 |
| mean anomaly at epoch: | 307.3796° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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