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 45441U 26145.38637645 +.00000000 +00000-0 -14029-2 0 00000
2 45441 87.8916 25.5937 0001890 80.7288 279.4053 13.11417070 06
| Epoch (UTC): | 25 May 2026 09:16:22 |
| Eccentricity: | 0.0001890 |
| inclination: | 87.8916° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5937° |
| argument of perigee: | 80.7288° |
| revolutions per day: | 13.11417070 |
| mean anomaly at epoch: | 279.4053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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