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 22178.29005694 .00000623 00000-0 12676-3 0 9995
2 28895 98.1079 309.5172 0017971 109.4772 250.8375 14.64362398888853
| Epoch (UTC): | 27 June 2022 06:57:40 |
| Eccentricity: | 0.0017971 |
| inclination: | 98.1079° |
| perigee height: | 666 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 309.5172° |
| argument of perigee: | 109.4772° |
| revolutions per day: | 14.64362398 |
| mean anomaly at epoch: | 250.8375° |
| orbit number at epoch: | 88885 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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