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 11870U 80056B 25188.49623320 .00000086 00000-0 36889-4 0 9991
2 11870 74.0511 201.4472 0015185 145.4612 214.7532 14.38206581333641
| Epoch (UTC): | 07 July 2025 11:54:34 |
| Eccentricity: | 0.0015185 |
| inclination: | 74.0511° |
| perigee height: | 753 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 201.4472° |
| argument of perigee: | 145.4612° |
| revolutions per day: | 14.38206581 |
| mean anomaly at epoch: | 214.7532° |
| orbit number at epoch: | 33364 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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