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 36508U 10013A 25191.58329517 .00000181 00000-0 44274-4 0 9990
2 36508 92.0089 194.7353 0002535 82.3661 277.7834 14.51910837808514
| Epoch (UTC): | 10 July 2025 13:59:56 |
| Eccentricity: | 0.0002535 |
| inclination: | 92.0089° |
| perigee height: | 717 km |
| apogee height: | 721 km |
| right ascension of ascending node: | 194.7353° |
| argument of perigee: | 82.3661° |
| revolutions per day: | 14.51910837 |
| mean anomaly at epoch: | 277.7834° |
| orbit number at epoch: | 80851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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