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 68253U 26144.86010014 +.00000000 +00000-0 +10986-2 0 00000
2 68253 53.1576 299.5481 0001018 62.8123 297.2989 15.49326595 08
| Epoch (UTC): | 24 May 2026 20:38:32 |
| Eccentricity: | 0.0001018 |
| inclination: | 53.1576° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 299.5481° |
| argument of perigee: | 62.8123° |
| revolutions per day: | 15.49326595 |
| mean anomaly at epoch: | 297.2989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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