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 00116U 26088.16333970 +.00000000 +00000-0 +95464-4 0 00009
2 00116 66.8076 86.6456 0079400 324.9357 34.6510 13.92316121 09
| Epoch (UTC): | 29 March 2026 03:55:12 |
| Eccentricity: | 0.0079400 |
| inclination: | 66.8076° |
| perigee height: | 863 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 86.6456° |
| argument of perigee: | 324.9357° |
| revolutions per day: | 13.92316121 |
| mean anomaly at epoch: | 34.6510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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