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 68374U 26145.19634747 +.00000000 +00000-0 +29320-3 0 00009
2 68374 82.2977 38.1505 0006298 173.4596 186.6756 15.84405018 02
| Epoch (UTC): | 25 May 2026 04:42:44 |
| Eccentricity: | 0.0006298 |
| inclination: | 82.2977° |
| perigee height: | 314 km |
| apogee height: | 322 km |
| right ascension of ascending node: | 38.1505° |
| argument of perigee: | 173.4596° |
| revolutions per day: | 15.84405018 |
| mean anomaly at epoch: | 186.6756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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