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 68070U 26145.49584865 +.00000000 +00000-0 +85010-3 0 00008
2 68070 53.1594 179.1496 0001226 71.2871 288.8264 15.34397956 04
| Epoch (UTC): | 25 May 2026 11:54:01 |
| Eccentricity: | 0.0001226 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 179.1496° |
| argument of perigee: | 71.2871° |
| revolutions per day: | 15.34397956 |
| mean anomaly at epoch: | 288.8264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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