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 68550U 26145.32391760 +.00000000 +00000-0 +93797-3 0 00004
2 68550 53.1605 6.2147 0001211 61.7059 298.4066 15.34409477 08
| Epoch (UTC): | 25 May 2026 07:46:26 |
| Eccentricity: | 0.0001211 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 6.2147° |
| argument of perigee: | 61.7059° |
| revolutions per day: | 15.34409477 |
| mean anomaly at epoch: | 298.4066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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