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 61853U 26145.53717707 +.00000000 +00000-0 -51117-4 0 00001
2 61853 43.0000 163.7208 0001476 263.8263 96.2420 15.27558258 08
| Epoch (UTC): | 25 May 2026 12:53:32 |
| Eccentricity: | 0.0001476 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 163.7208° |
| argument of perigee: | 263.8263° |
| revolutions per day: | 15.27558258 |
| mean anomaly at epoch: | 96.2420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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