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 68066U 26145.58335647 +.00000000 +00000-0 +16961-2 0 00003
2 68066 53.1598 50.7144 0000643 95.8171 102.8002 15.34355903 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000643 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 50.7144° |
| argument of perigee: | 95.8171° |
| revolutions per day: | 15.34355903 |
| mean anomaly at epoch: | 102.8002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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