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 45807U 26145.60563279 +.00000000 +00000-0 +00000-0 0 00003
2 45807 2.3943 67.4031 0003163 335.6353 168.6958 1.00268426 01
| Epoch (UTC): | 25 May 2026 14:32:06 |
| Eccentricity: | 0.0003163 |
| inclination: | 2.3943° |
| perigee height: | 35774 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 67.4031° |
| argument of perigee: | 335.6353° |
| revolutions per day: | 1.00268426 |
| mean anomaly at epoch: | 168.6958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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