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 68007U 26145.59027567 +.00000000 +00000-0 +63073-3 0 00005
2 68007 43.0030 334.6909 0001644 248.4755 111.5922 15.27594262 01
| Epoch (UTC): | 25 May 2026 14:09:59 |
| Eccentricity: | 0.0001644 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 334.6909° |
| argument of perigee: | 248.4755° |
| revolutions per day: | 15.27594262 |
| mean anomaly at epoch: | 111.5922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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