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 63133U 26145.47318189 +.00000000 +00000-0 +15815-2 0 00000
2 63133 43.0011 148.2992 0001796 254.8232 105.2438 15.70893274 00
| Epoch (UTC): | 25 May 2026 11:21:22 |
| Eccentricity: | 0.0001796 |
| inclination: | 43.0011° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 148.2992° |
| argument of perigee: | 254.8232° |
| revolutions per day: | 15.70893274 |
| mean anomaly at epoch: | 105.2438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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