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 11416U 26022.47571461 +.00000000 +00000-0 +23066-3 0 00003
2 11416 98.5804 52.8993 0009290 336.3394 23.7363 14.35392564 02
| Epoch (UTC): | 22 January 2026 11:25:01 |
| Eccentricity: | 0.0009290 |
| inclination: | 98.5804° |
| perigee height: | 767 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 52.8993° |
| argument of perigee: | 336.3394° |
| revolutions per day: | 14.35392564 |
| mean anomaly at epoch: | 23.7363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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