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 63081U 26145.43440625 +.00000000 +00000-0 +32141-3 0 00001
2 63081 70.0004 161.1168 0004423 265.6387 94.4267 14.98331357 01
| Epoch (UTC): | 25 May 2026 10:25:32 |
| Eccentricity: | 0.0004423 |
| inclination: | 70.0004° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 161.1168° |
| argument of perigee: | 265.6387° |
| revolutions per day: | 14.98331357 |
| mean anomaly at epoch: | 94.4267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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