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 68699U 26145.58335647 +.00000000 +00000-0 -31353-1 0 00007
2 68699 53.1597 37.3085 0000755 92.2757 147.7275 15.36100130 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000755 |
| inclination: | 53.1597° |
| perigee height: | 457 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 37.3085° |
| argument of perigee: | 92.2757° |
| revolutions per day: | 15.36100130 |
| mean anomaly at epoch: | 147.7275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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