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 63601U 26145.60258138 +.00000000 +00000-0 +11629-3 0 00002
2 63601 99.6907 153.2351 0001129 95.2150 264.9117 13.57243994 00
| Epoch (UTC): | 25 May 2026 14:27:43 |
| Eccentricity: | 0.0001129 |
| inclination: | 99.6907° |
| perigee height: | 1045 km |
| apogee height: | 1047 km |
| right ascension of ascending node: | 153.2351° |
| argument of perigee: | 95.2150° |
| revolutions per day: | 13.57243994 |
| mean anomaly at epoch: | 264.9117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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