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 38070U 26145.60123441 +.00000000 +00000-0 +00000-0 0 00000
2 38070 0.0150 311.8045 0000978 338.5893 257.6551 1.00268009 08
| Epoch (UTC): | 25 May 2026 14:25:46 |
| Eccentricity: | 0.0000978 |
| inclination: | 0.0150° |
| perigee height: | 35784 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 311.8045° |
| argument of perigee: | 338.5893° |
| revolutions per day: | 1.00268009 |
| mean anomaly at epoch: | 257.6551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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