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 45427U 26145.40021832 +.00000000 +00000-0 -71520-3 0 00002
2 45427 87.8920 25.6038 0001718 81.6137 278.5186 13.11418239 05
| Epoch (UTC): | 25 May 2026 09:36:18 |
| Eccentricity: | 0.0001718 |
| inclination: | 87.8920° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6038° |
| argument of perigee: | 81.6137° |
| revolutions per day: | 13.11418239 |
| mean anomaly at epoch: | 278.5186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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