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 25336.22448648 0.00000000 00000-0 00000-0 0 00
2 37391 63.4218 64.5097 0324053 358.6119 1.3881 13.40979051 00
| Epoch (UTC): | 02 December 2025 05:23:15 |
| Eccentricity: | 0.0324053 |
| inclination: | 63.4218° |
| perigee height: | 863 km |
| apogee height: | 1348 km |
| right ascension of ascending node: | 64.5097° |
| argument of perigee: | 358.6119° |
| revolutions per day: | 13.40979051 |
| mean anomaly at epoch: | 1.3881° |
| 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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