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 68925U 26145.38305662 +.00000000 +00000-0 +59007-3 0 00008
2 68925 51.8728 177.6667 0008138 65.8536 294.3299 15.34170337 08
| Epoch (UTC): | 25 May 2026 09:11:36 |
| Eccentricity: | 0.0008138 |
| inclination: | 51.8728° |
| perigee height: | 458 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 177.6667° |
| argument of perigee: | 65.8536° |
| revolutions per day: | 15.34170337 |
| mean anomaly at epoch: | 294.3299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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