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 28096U 03054B 23126.10201099 0.00000000 00000-0 00000-0 0 06
2 28096 63.6728 28.4082 0155842 190.4747 169.5253 13.40920573 05
| Epoch (UTC): | 06 May 2023 02:26:53 |
| Eccentricity: | 0.0155842 |
| inclination: | 63.6728° |
| perigee height: | 989 km |
| apogee height: | 1222 km |
| right ascension of ascending node: | 28.4082° |
| argument of perigee: | 190.4747° |
| revolutions per day: | 13.40920573 |
| mean anomaly at epoch: | 169.5253° |
| 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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