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 25198.45938124 .00000422 00000-0 11767-3 0 9994
2 36416 63.3902 233.5189 0669444 1.0774 359.1530 13.72210310768825
| Epoch (UTC): | 17 July 2025 11:01:30 |
| Eccentricity: | 0.0669444 |
| inclination: | 63.3902° |
| perigee height: | 498 km |
| apogee height: | 1485 km |
| right ascension of ascending node: | 233.5189° |
| argument of perigee: | 1.0774° |
| revolutions per day: | 13.72210310 |
| mean anomaly at epoch: | 359.1530° |
| orbit number at epoch: | 76882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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