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 26069.99551022 +.00000000 +00000-0 +24361-3 0 00000
2 32953 82.5005 56.5100 0019574 162.3584 197.8179 12.43176031 06
| Epoch (UTC): | 10 March 2026 23:53:32 |
| Eccentricity: | 0.0019574 |
| inclination: | 82.5005° |
| perigee height: | 1478 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 56.5100° |
| argument of perigee: | 162.3584° |
| revolutions per day: | 12.43176031 |
| mean anomaly at epoch: | 197.8179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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