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 32376U 26071.95852399 +.00000000 +00000-0 +91344-4 0 00005
2 32376 97.8872 256.9473 0001334 83.6213 276.5152 14.82147786 00
| Epoch (UTC): | 12 March 2026 23:00:16 |
| Eccentricity: | 0.0001334 |
| inclination: | 97.8872° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 256.9473° |
| argument of perigee: | 83.6213° |
| revolutions per day: | 14.82147786 |
| mean anomaly at epoch: | 276.5152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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