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 68985U 26145.26810652 +.00000000 +00000-0 +15226-3 0 00006
2 68985 97.7394 43.1503 0001973 154.8738 205.2578 14.91670066 08
| Epoch (UTC): | 25 May 2026 06:26:04 |
| Eccentricity: | 0.0001973 |
| inclination: | 97.7394° |
| perigee height: | 591 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 43.1503° |
| argument of perigee: | 154.8738° |
| revolutions per day: | 14.91670066 |
| mean anomaly at epoch: | 205.2578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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