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 28097U 03054C 23075.77971357 0.00000400 00000-0 35839-3 0 09
2 28097 63.4055 355.0544 0487865 1.6033 358.3967 13.40850799 05
| Epoch (UTC): | 16 March 2023 18:42:47 |
| Eccentricity: | 0.0487865 |
| inclination: | 63.4055° |
| perigee height: | 741 km |
| apogee height: | 1471 km |
| right ascension of ascending node: | 355.0544° |
| argument of perigee: | 1.6033° |
| revolutions per day: | 13.40850799 |
| mean anomaly at epoch: | 358.3967° |
| 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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