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 68890U 26144.99356031 +.00000000 +00000-0 +69186-3 0 00000
2 68890 51.8834 354.3449 0001879 165.4705 194.6337 15.38694248 00
| Epoch (UTC): | 24 May 2026 23:50:43 |
| Eccentricity: | 0.0001879 |
| inclination: | 51.8834° |
| perigee height: | 449 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 354.3449° |
| argument of perigee: | 165.4705° |
| revolutions per day: | 15.38694248 |
| mean anomaly at epoch: | 194.6337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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