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 45136U 26145.47012023 +.00000000 +00000-0 +17055-2 0 00009
2 45136 87.8856 40.7865 0001960 81.0710 279.0639 13.10372592 05
| Epoch (UTC): | 25 May 2026 11:16:58 |
| Eccentricity: | 0.0001960 |
| inclination: | 87.8856° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7865° |
| argument of perigee: | 81.0710° |
| revolutions per day: | 13.10372592 |
| mean anomaly at epoch: | 279.0639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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