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 22138.58940433 .00001605 00000-0 31286-3 0 9991
2 28895 98.1022 270.4364 0015667 232.2538 127.7246 14.64285053883277
| Epoch (UTC): | 18 May 2022 14:08:44 |
| Eccentricity: | 0.0015667 |
| inclination: | 98.1022° |
| perigee height: | 668 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 270.4364° |
| argument of perigee: | 232.2538° |
| revolutions per day: | 14.64285053 |
| mean anomaly at epoch: | 127.7246° |
| orbit number at epoch: | 88327 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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