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 68096U 26145.38930164 +.00000000 +00000-0 +37802-3 0 00007
2 68096 53.1581 182.0717 0001385 102.6875 257.4282 15.34375838 03
| Epoch (UTC): | 25 May 2026 09:20:35 |
| Eccentricity: | 0.0001385 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 182.0717° |
| argument of perigee: | 102.6875° |
| revolutions per day: | 15.34375838 |
| mean anomaly at epoch: | 257.4282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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