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 68041U 26145.16083039 +.00000000 +00000-0 +12523-2 0 00005
2 68041 53.1585 52.7301 0001090 96.8207 263.2920 15.34405145 04
| Epoch (UTC): | 25 May 2026 03:51:35 |
| Eccentricity: | 0.0001090 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 52.7301° |
| argument of perigee: | 96.8207° |
| revolutions per day: | 15.34405145 |
| mean anomaly at epoch: | 263.2920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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