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 37391U 11014B 23087.84372767 0.00000000 00000-0 00000-0 0 07
2 37391 63.4338 42.1903 0253525 357.3227 2.6773 13.40862818 08
| Epoch (UTC): | 28 March 2023 20:14:58 |
| Eccentricity: | 0.0253525 |
| inclination: | 63.4338° |
| perigee height: | 916 km |
| apogee height: | 1296 km |
| right ascension of ascending node: | 42.1903° |
| argument of perigee: | 357.3227° |
| revolutions per day: | 13.40862818 |
| mean anomaly at epoch: | 2.6773° |
| 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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