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 68865U 26144.99054012 +.00000000 +00000-0 +12990-2 0 00006
2 68865 51.8863 354.3218 0001048 223.1515 136.9390 15.38733357 00
| Epoch (UTC): | 24 May 2026 23:46:22 |
| Eccentricity: | 0.0001048 |
| inclination: | 51.8863° |
| perigee height: | 449 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 354.3218° |
| argument of perigee: | 223.1515° |
| revolutions per day: | 15.38733357 |
| mean anomaly at epoch: | 136.9390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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