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 68924U 26145.48606682 +.00000000 +00000-0 +69588-4 0 00000
2 68924 51.8758 177.5999 0015630 66.9920 293.2711 15.30584069 05
| Epoch (UTC): | 25 May 2026 11:39:56 |
| Eccentricity: | 0.0015630 |
| inclination: | 51.8758° |
| perigee height: | 463 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 177.5999° |
| argument of perigee: | 66.9920° |
| revolutions per day: | 15.30584069 |
| mean anomaly at epoch: | 293.2711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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