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 45663U 26145.61014167 +.00000000 +00000-0 +42042-3 0 00006
2 45663 53.0232 352.9797 0004053 131.4528 228.6826 15.46571530 00
| Epoch (UTC): | 25 May 2026 14:38:36 |
| Eccentricity: | 0.0004053 |
| inclination: | 53.0232° |
| perigee height: | 424 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 352.9797° |
| argument of perigee: | 131.4528° |
| revolutions per day: | 15.46571530 |
| mean anomaly at epoch: | 228.6826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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