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 22175.35186499 .00000727 00000-0 14634-3 0 9993
2 28895 98.1075 306.6239 0017897 118.0808 242.2207 14.64358128888422
| Epoch (UTC): | 24 June 2022 08:26:41 |
| Eccentricity: | 0.0017897 |
| inclination: | 98.1075° |
| perigee height: | 666 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 306.6239° |
| argument of perigee: | 118.0808° |
| revolutions per day: | 14.64358128 |
| mean anomaly at epoch: | 242.2207° |
| orbit number at epoch: | 88842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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