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 28895U 05043F 23091.12434794 .00003443 00000-0 64565-3 0 9996
2 28895 98.1395 223.8458 0015368 317.7535 42.2484 14.65326396929756
| Epoch (UTC): | 01 April 2023 02:59:03 |
| Eccentricity: | 0.0015368 |
| inclination: | 98.1395° |
| perigee height: | 665 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 223.8458° |
| argument of perigee: | 317.7535° |
| revolutions per day: | 14.65326396 |
| mean anomaly at epoch: | 42.2484° |
| orbit number at epoch: | 92975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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