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 32953U 26101.30161748 +.00000000 +00000-0 +62151-3 0 00003
2 32953 82.5060 37.0365 0020546 96.0360 264.3062 12.43177697 00
| Epoch (UTC): | 11 April 2026 07:14:19 |
| Eccentricity: | 0.0020546 |
| inclination: | 82.5060° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 37.0365° |
| argument of perigee: | 96.0360° |
| revolutions per day: | 12.43177697 |
| mean anomaly at epoch: | 264.3062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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