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 26088.06899697 +.00000000 +00000-0 +13340-3 0 00008
2 11416 98.5721 118.1029 0010765 131.7954 228.4152 14.35447708 05
| Epoch (UTC): | 29 March 2026 01:39:21 |
| Eccentricity: | 0.0010765 |
| inclination: | 98.5721° |
| perigee height: | 766 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 118.1029° |
| argument of perigee: | 131.7954° |
| revolutions per day: | 14.35447708 |
| mean anomaly at epoch: | 228.4152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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