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 27006U 01056F 25118.71903510 -.00000016 00000-0 34159-4 0 9994
2 27006 99.7307 275.0470 0015308 77.3515 293.3398 13.71073669170033
| Epoch (UTC): | 28 April 2025 17:15:24 |
| Eccentricity: | 0.0015308 |
| inclination: | 99.7307° |
| perigee height: | 984 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 275.0470° |
| argument of perigee: | 77.3515° |
| revolutions per day: | 13.71073669 |
| mean anomaly at epoch: | 293.3398° |
| orbit number at epoch: | 17003 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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