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 68097U 26145.50483081 +.00000000 +00000-0 +83851-3 0 00008
2 68097 53.1594 181.3800 0000946 81.3684 278.7426 15.34398107 06
| Epoch (UTC): | 25 May 2026 12:06:57 |
| Eccentricity: | 0.0000946 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 181.3800° |
| argument of perigee: | 81.3684° |
| revolutions per day: | 15.34398107 |
| mean anomaly at epoch: | 278.7426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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