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 28097U 03054C 22128.87955208 0.00000000 00000-0 00000-0 0 00
2 28097 63.4050 73.2962 0461535 0.5846 359.4154 13.40796715 06
| Epoch (UTC): | 08 May 2022 21:06:33 |
| Eccentricity: | 0.0461535 |
| inclination: | 63.4050° |
| perigee height: | 761 km |
| apogee height: | 1452 km |
| right ascension of ascending node: | 73.2962° |
| argument of perigee: | 0.5846° |
| revolutions per day: | 13.40796715 |
| mean anomaly at epoch: | 359.4154° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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