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 45452U 26145.59676352 +.00000000 +00000-0 -14556-3 0 00009
2 45452 87.8917 25.5521 0001899 75.0253 285.1085 13.11414243 04
| Epoch (UTC): | 25 May 2026 14:19:20 |
| Eccentricity: | 0.0001899 |
| inclination: | 87.8917° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5521° |
| argument of perigee: | 75.0253° |
| revolutions per day: | 13.11414243 |
| mean anomaly at epoch: | 285.1085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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