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 36095U 09063A 25136.38450924 -.00000042 00000-0 23919-4 0 9998
2 36095 67.1454 137.8850 0004973 298.2293 61.8289 13.97001174789700
| Epoch (UTC): | 16 May 2025 09:13:41 |
| Eccentricity: | 0.0004973 |
| inclination: | 67.1454° |
| perigee height: | 900 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 137.8850° |
| argument of perigee: | 298.2293° |
| revolutions per day: | 13.97001174 |
| mean anomaly at epoch: | 61.8289° |
| orbit number at epoch: | 78970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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