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 23151.14049140 .00001493 00000-0 28325-3 0 9999
2 28895 98.1514 283.3333 0017452 124.1392 236.1469 14.65611173938543
| Epoch (UTC): | 31 May 2023 03:22:18 |
| Eccentricity: | 0.0017452 |
| inclination: | 98.1514° |
| perigee height: | 663 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 283.3333° |
| argument of perigee: | 124.1392° |
| revolutions per day: | 14.65611173 |
| mean anomaly at epoch: | 236.1469° |
| orbit number at epoch: | 93854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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