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 61540U 26145.35603670 +.00000000 +00000-0 +75464-5 0 00008
2 61540 53.1594 217.9553 0000874 5.5551 354.5476 15.69691124 05
| Epoch (UTC): | 25 May 2026 08:32:41 |
| Eccentricity: | 0.0000874 |
| inclination: | 53.1594° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 217.9553° |
| argument of perigee: | 5.5551° |
| revolutions per day: | 15.69691124 |
| mean anomaly at epoch: | 354.5476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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