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 68116U 26145.61527207 +.00000000 +00000-0 +63007-3 0 00002
2 68116 97.2844 106.2644 0001678 104.9980 255.1449 15.33447747 09
| Epoch (UTC): | 25 May 2026 14:45:59 |
| Eccentricity: | 0.0001678 |
| inclination: | 97.2844° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 106.2644° |
| argument of perigee: | 104.9980° |
| revolutions per day: | 15.33447747 |
| mean anomaly at epoch: | 255.1449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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