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 36416U 10009D 25191.53623036 .00000254 00000-0 83212-4 0 9997
2 36416 63.3915 252.3111 0668715 1.0353 359.1896 13.72203369767680
| Epoch (UTC): | 10 July 2025 12:52:10 |
| Eccentricity: | 0.0668715 |
| inclination: | 63.3915° |
| perigee height: | 499 km |
| apogee height: | 1484 km |
| right ascension of ascending node: | 252.3111° |
| argument of perigee: | 1.0353° |
| revolutions per day: | 13.72203369 |
| mean anomaly at epoch: | 359.1896° |
| orbit number at epoch: | 76768 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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