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 68396U 26145.65658162 +.00000000 +00000-0 +18588-3 0 00005
2 68396 97.2862 288.2584 0002795 98.4532 261.7028 15.33450438 01
| Epoch (UTC): | 25 May 2026 15:45:28 |
| Eccentricity: | 0.0002795 |
| inclination: | 97.2862° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 288.2584° |
| argument of perigee: | 98.4532° |
| revolutions per day: | 15.33450438 |
| mean anomaly at epoch: | 261.7028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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