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 23126.11375670 0.00000000 00000-0 00000-0 0 02
2 31708 63.3843 358.4743 0375587 20.5718 339.4282 13.40882377 04
| Epoch (UTC): | 06 May 2023 02:43:48 |
| Eccentricity: | 0.0375587 |
| inclination: | 63.3843° |
| perigee height: | 825 km |
| apogee height: | 1387 km |
| right ascension of ascending node: | 358.4743° |
| argument of perigee: | 20.5718° |
| revolutions per day: | 13.40882377 |
| mean anomaly at epoch: | 339.4282° |
| 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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