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 26057.27990279 +.00000000 +00000-0 -44958-3 0 00004
2 32953 82.4991 64.4245 0019100 190.2172 169.8522 12.43175102 04
| Epoch (UTC): | 26 February 2026 06:43:03 |
| Eccentricity: | 0.0019100 |
| inclination: | 82.4991° |
| perigee height: | 1478 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 64.4245° |
| argument of perigee: | 190.2172° |
| revolutions per day: | 12.43175102 |
| mean anomaly at epoch: | 169.8522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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