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 16631U 86014H 25188.61442931 .00008836 00000-0 51018-3 0 9993
2 16631 63.2928 276.8354 0797914 105.7836 263.2603 13.84818288296506
| Epoch (UTC): | 07 July 2025 14:44:46 |
| Eccentricity: | 0.0797914 |
| inclination: | 63.2928° |
| perigee height: | 362 km |
| apogee height: | 1531 km |
| right ascension of ascending node: | 276.8354° |
| argument of perigee: | 105.7836° |
| revolutions per day: | 13.84818288 |
| mean anomaly at epoch: | 263.2603° |
| orbit number at epoch: | 29650 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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