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 68928U 26145.50809779 +.00000000 +00000-0 +24565-3 0 00004
2 68928 51.8733 177.7330 0025088 80.2398 280.1417 15.29733411 02
| Epoch (UTC): | 25 May 2026 12:11:39 |
| Eccentricity: | 0.0025088 |
| inclination: | 51.8733° |
| perigee height: | 459 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 177.7330° |
| argument of perigee: | 80.2398° |
| revolutions per day: | 15.29733411 |
| mean anomaly at epoch: | 280.1417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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