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 26073.53656483 +.00000000 +00000-0 +35438-3 0 00009
2 32953 82.5006 54.3066 0019695 154.7194 205.4854 12.43176204 08
| Epoch (UTC): | 14 March 2026 12:52:39 |
| Eccentricity: | 0.0019695 |
| inclination: | 82.5006° |
| perigee height: | 1478 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 54.3066° |
| argument of perigee: | 154.7194° |
| revolutions per day: | 12.43176204 |
| mean anomaly at epoch: | 205.4854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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