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 is defined by the following mean orbital elements,
1 36416U 26041.32478042 +.00000000 +00000-0 +45145-3 0 00008
2 36416 63.3892 28.8009 0687751 2.4495 357.9635 13.72853888 09
| Epoch (UTC): | 10 February 2026 07:47:41 |
| Eccentricity: | 0.0687751 |
| inclination: | 63.3892° |
| perigee height: | 483 km |
| apogee height: | 1496 km |
| right ascension of ascending node: | 28.8009° |
| argument of perigee: | 2.4495° |
| revolutions per day: | 13.72853888 |
| mean anomaly at epoch: | 357.9635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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