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 data is extracted from the following two-line orbital elements,
1 31708U 07027C 25189.95209849 0.00000128 00000-0 13156-3 0 09
2 31708 63.3748 125.1519 0437346 22.7607 337.2393 13.40967371 08
| Epoch (UTC): | 08 July 2025 22:51:01 |
| Eccentricity: | 0.0437346 |
| inclination: | 63.3748° |
| perigee height: | 778 km |
| apogee height: | 1433 km |
| right ascension of ascending node: | 125.1519° |
| argument of perigee: | 22.7607° |
| revolutions per day: | 13.40967371 |
| mean anomaly at epoch: | 337.2393° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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