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 26038.26544545 +.00000000 +00000-0 +49175-3 0 00006
2 36416 63.3888 37.1195 0687437 2.4280 357.9821 13.72839510 09
| Epoch (UTC): | 07 February 2026 06:22:14 |
| Eccentricity: | 0.0687437 |
| inclination: | 63.3888° |
| perigee height: | 483 km |
| apogee height: | 1496 km |
| right ascension of ascending node: | 37.1195° |
| argument of perigee: | 2.4280° |
| revolutions per day: | 13.72839510 |
| mean anomaly at epoch: | 357.9821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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