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 25544U 26065.22200802 +.00000000 +00000-0 +15844-3 0 00003
2 25544 51.6317 89.5003 0008136 162.2758 197.8515 15.48470661 07
| Epoch (UTC): | 06 March 2026 05:19:41 |
| Eccentricity: | 0.0008136 |
| inclination: | 51.6317° |
| perigee height: | 416 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 89.5003° |
| argument of perigee: | 162.2758° |
| revolutions per day: | 15.48470661 |
| mean anomaly at epoch: | 197.8515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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