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 45149U 26145.44936547 +.00000000 +00000-0 +36281-4 0 00000
2 45149 87.8857 40.7922 0002390 76.0864 284.0529 13.10375167 01
| Epoch (UTC): | 25 May 2026 10:47:05 |
| Eccentricity: | 0.0002390 |
| inclination: | 87.8857° |
| perigee height: | 1220 km |
| apogee height: | 1224 km |
| right ascension of ascending node: | 40.7922° |
| argument of perigee: | 76.0864° |
| revolutions per day: | 13.10375167 |
| mean anomaly at epoch: | 284.0529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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