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 28894U 05043E 22222.30994512 .00000228 00000-0 54873-4 0 9999
2 28894 98.1298 346.2084 0017236 14.6057 345.5639 14.61933429894973
| Epoch (UTC): | 10 August 2022 07:26:19 |
| Eccentricity: | 0.0017236 |
| inclination: | 98.1298° |
| perigee height: | 675 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 346.2084° |
| argument of perigee: | 14.6057° |
| revolutions per day: | 14.61933429 |
| mean anomaly at epoch: | 345.5639° |
| orbit number at epoch: | 89497 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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