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 45445U 26145.59589505 +.00000000 +00000-0 -61366-4 0 00006
2 45445 87.8903 25.5643 0001950 79.2802 280.8545 13.10885423 04
| Epoch (UTC): | 25 May 2026 14:18:05 |
| Eccentricity: | 0.0001950 |
| inclination: | 87.8903° |
| perigee height: | 1218 km |
| apogee height: | 1221 km |
| right ascension of ascending node: | 25.5643° |
| argument of perigee: | 79.2802° |
| revolutions per day: | 13.10885423 |
| mean anomaly at epoch: | 280.8545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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