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 61602U 26145.37972412 +.00000000 +00000-0 -12001-2 0 00008
2 61602 87.8907 25.6147 0001466 97.1886 262.9409 13.11414863 01
| Epoch (UTC): | 25 May 2026 09:06:48 |
| Eccentricity: | 0.0001466 |
| inclination: | 87.8907° |
| perigee height: | 1217 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6147° |
| argument of perigee: | 97.1886° |
| revolutions per day: | 13.11414863 |
| mean anomaly at epoch: | 262.9409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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