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 63165U 26145.54470325 +.00000000 +00000-0 +12182-3 0 00009
2 63165 88.9694 303.1222 0015127 22.5353 337.6459 13.51007252 09
| Epoch (UTC): | 25 May 2026 13:04:22 |
| Eccentricity: | 0.0015127 |
| inclination: | 88.9694° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 303.1222° |
| argument of perigee: | 22.5353° |
| revolutions per day: | 13.51007252 |
| mean anomaly at epoch: | 337.6459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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