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 63162U 26145.54875337 +.00000000 +00000-0 +22198-3 0 00006
2 63162 88.9692 303.1458 0013932 22.6209 337.5553 13.51008579 05
| Epoch (UTC): | 25 May 2026 13:10:12 |
| Eccentricity: | 0.0013932 |
| inclination: | 88.9692° |
| perigee height: | 1058 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 303.1458° |
| argument of perigee: | 22.6209° |
| revolutions per day: | 13.51008579 |
| mean anomaly at epoch: | 337.5553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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