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 23273.32837073 .00002780 00000-0 51401-3 0 9995
2 28895 98.1681 44.6946 0017298 100.7023 259.6129 14.66099829956446
| Epoch (UTC): | 30 September 2023 07:52:51 |
| Eccentricity: | 0.0017298 |
| inclination: | 98.1681° |
| perigee height: | 661 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 44.6946° |
| argument of perigee: | 100.7023° |
| revolutions per day: | 14.66099829 |
| mean anomaly at epoch: | 259.6129° |
| orbit number at epoch: | 95644 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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