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 45087U 26145.63884117 +.00000000 +00000-0 +10021-2 0 00009
2 45087 53.1591 239.8580 0004279 334.9438 25.1361 15.44331807 05
| Epoch (UTC): | 25 May 2026 15:19:55 |
| Eccentricity: | 0.0004279 |
| inclination: | 53.1591° |
| perigee height: | 430 km |
| apogee height: | 436 km |
| right ascension of ascending node: | 239.8580° |
| argument of perigee: | 334.9438° |
| revolutions per day: | 15.44331807 |
| mean anomaly at epoch: | 25.1361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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