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 22178.90502643 .00000526 00000-0 10832-3 0 9993
2 28895 98.1081 310.1228 0017986 107.6833 252.6335 14.64362733888949
| Epoch (UTC): | 27 June 2022 21:43:14 |
| Eccentricity: | 0.0017986 |
| inclination: | 98.1081° |
| perigee height: | 666 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 310.1228° |
| argument of perigee: | 107.6833° |
| revolutions per day: | 14.64362733 |
| mean anomaly at epoch: | 252.6335° |
| orbit number at epoch: | 88894 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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