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 42907U 26144.80844419 +.00000000 +00000-0 +00000-0 0 00000
2 42907 0.0150 61.0936 0001075 70.4175 86.9343 1.00269687 04
| Epoch (UTC): | 24 May 2026 19:24:09 |
| Eccentricity: | 0.0001075 |
| inclination: | 0.0150° |
| perigee height: | 35783 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 61.0936° |
| argument of perigee: | 70.4175° |
| revolutions per day: | 1.00269687 |
| mean anomaly at epoch: | 86.9343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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