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 is defined by the following mean orbital elements,
1 48275U 21035B 21128.85708450 .10495065 80719-5 19011-3 0 9993
2 48275 41.4573 159.7603 0029099 247.8635 292.7779 16.44362448 1542
| Epoch (UTC): | 08 May 2021 20:34:12 |
| Eccentricity: | 0.0029099 |
| inclination: | 41.4573° |
| perigee height: | 135 km |
| apogee height: | 173 km |
| right ascension of ascending node: | 159.7603° |
| argument of perigee: | 247.8635° |
| revolutions per day: | 16.44362448 |
| mean anomaly at epoch: | 292.7779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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