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 61954U 26145.39828882 +.00000000 +00000-0 +72436-3 0 00009
2 61954 53.1585 143.8044 0001476 93.3980 266.7195 15.42182676 06
| Epoch (UTC): | 25 May 2026 09:33:32 |
| Eccentricity: | 0.0001476 |
| inclination: | 53.1585° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 143.8044° |
| argument of perigee: | 93.3980° |
| revolutions per day: | 15.42182676 |
| mean anomaly at epoch: | 266.7195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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