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 37841U 11058D 23090.33416667 .00000619 00000-0 19461-3 0 9998
2 37841 19.9730 320.7195 0011821 256.0943 74.6144 14.10863486592028
| Epoch (UTC): | 31 March 2023 08:01:12 |
| Eccentricity: | 0.0011821 |
| inclination: | 19.9730° |
| perigee height: | 848 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 320.7195° |
| argument of perigee: | 256.0943° |
| revolutions per day: | 14.10863486 |
| mean anomaly at epoch: | 74.6144° |
| orbit number at epoch: | 59202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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