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 01314U 65027A 23030.38813642 .00000028 00000-0 78794-4 0 9991
2 01314 90.2609 338.9008 0028582 267.7505 207.1207 12.91770617471737
| Epoch (UTC): | 30 January 2023 09:18:54 |
| Eccentricity: | 0.0028582 |
| inclination: | 90.2609° |
| perigee height: | 1272 km |
| apogee height: | 1316 km |
| right ascension of ascending node: | 338.9008° |
| argument of perigee: | 267.7505° |
| revolutions per day: | 12.91770617 |
| mean anomaly at epoch: | 207.1207° |
| orbit number at epoch: | 47173 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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