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 61554U 26145.55478413 +.00000000 +00000-0 +22231-3 0 00002
2 61554 88.9768 57.7807 0010057 176.5021 183.6243 14.22827285 06
| Epoch (UTC): | 25 May 2026 13:18:53 |
| Eccentricity: | 0.0010057 |
| inclination: | 88.9768° |
| perigee height: | 809 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 57.7807° |
| argument of perigee: | 176.5021° |
| revolutions per day: | 14.22827285 |
| mean anomaly at epoch: | 183.6243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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