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 68263U 26145.50634944 +.00000000 +00000-0 +70536-3 0 00005
2 68263 53.1569 323.0539 0000474 8.2075 351.8935 15.34403991 01
| Epoch (UTC): | 25 May 2026 12:09:08 |
| Eccentricity: | 0.0000474 |
| inclination: | 53.1569° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 323.0539° |
| argument of perigee: | 8.2075° |
| revolutions per day: | 15.34403991 |
| mean anomaly at epoch: | 351.8935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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