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 12786U 81082B 24357.79945765 .00000956 00000-0 10519-3 0 9995
2 12786 82.4883 258.5482 0016657 181.5944 178.5222 14.86469481321206
| Epoch (UTC): | 22 December 2024 19:11:13 |
| Eccentricity: | 0.0016657 |
| inclination: | 82.4883° |
| perigee height: | 597 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 258.5482° |
| argument of perigee: | 181.5944° |
| revolutions per day: | 14.86469481 |
| mean anomaly at epoch: | 178.5222° |
| orbit number at epoch: | 32120 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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