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 45986U 26145.10356119 +.00000000 +00000-0 +00000-0 0 00009
2 45986 0.0262 285.5525 0001863 263.4341 171.0069 1.00272757 02
| Epoch (UTC): | 25 May 2026 02:29:07 |
| Eccentricity: | 0.0001863 |
| inclination: | 0.0262° |
| perigee height: | 35778 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 285.5525° |
| argument of perigee: | 263.4341° |
| revolutions per day: | 1.00272757 |
| mean anomaly at epoch: | 171.0069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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