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 68923U 26145.47731273 +.00000000 +00000-0 +44420-3 0 00000
2 68923 51.8764 177.5448 0015010 67.4562 292.8009 15.32072966 05
| Epoch (UTC): | 25 May 2026 11:27:19 |
| Eccentricity: | 0.0015010 |
| inclination: | 51.8764° |
| perigee height: | 459 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 177.5448° |
| argument of perigee: | 67.4562° |
| revolutions per day: | 15.32072966 |
| mean anomaly at epoch: | 292.8009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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