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 68970U 26145.58335647 +.00000000 +00000-0 -25531-1 0 00000
2 68970 53.1593 268.0392 0001173 58.1754 60.0529 15.60741592 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001173 |
| inclination: | 53.1593° |
| perigee height: | 385 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 268.0392° |
| argument of perigee: | 58.1754° |
| revolutions per day: | 15.60741592 |
| mean anomaly at epoch: | 60.0529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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