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 24354.72860682 0.00000000 00000-0 00000-0 0 00
2 37391 63.4312 231.0460 0305499 356.5315 3.4685 13.40949396 02
| Epoch (UTC): | 19 December 2024 17:29:11 |
| Eccentricity: | 0.0305499 |
| inclination: | 63.4312° |
| perigee height: | 877 km |
| apogee height: | 1334 km |
| right ascension of ascending node: | 231.0460° |
| argument of perigee: | 356.5315° |
| revolutions per day: | 13.40949396 |
| mean anomaly at epoch: | 3.4685° |
| 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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