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 68736U 26145.58335647 +.00000000 +00000-0 -33712-1 0 00000
2 68736 97.2847 9.2235 0001419 104.2218 212.4724 15.56017712 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001419 |
| inclination: | 97.2847° |
| perigee height: | 398 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 9.2235° |
| argument of perigee: | 104.2218° |
| revolutions per day: | 15.56017712 |
| mean anomaly at epoch: | 212.4724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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