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 63671U 26145.51634551 +.00000000 +00000-0 +12032-2 0 00004
2 63671 43.0029 175.4222 0001781 266.6476 93.4188 15.70907765 00
| Epoch (UTC): | 25 May 2026 12:23:32 |
| Eccentricity: | 0.0001781 |
| inclination: | 43.0029° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 175.4222° |
| argument of perigee: | 266.6476° |
| revolutions per day: | 15.70907765 |
| mean anomaly at epoch: | 93.4188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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