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 26104.11017201 +.00000000 +00000-0 +70300-4 0 00001
2 00116 66.8106 47.6237 0080362 314.4211 45.0309 13.92320840 04
| Epoch (UTC): | 14 April 2026 02:38:38 |
| Eccentricity: | 0.0080362 |
| inclination: | 66.8106° |
| perigee height: | 862 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 47.6237° |
| argument of perigee: | 314.4211° |
| revolutions per day: | 13.92320840 |
| mean anomaly at epoch: | 45.0309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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