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 26157.29183074 +.00000000 +00000-0 +68572-4 0 00001
2 32376 97.8885 341.0480 0001439 87.7342 272.4035 14.82162786 04
| Epoch (UTC): | 06 June 2026 07:00:14 |
| Eccentricity: | 0.0001439 |
| inclination: | 97.8885° |
| perigee height: | 621 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 341.0480° |
| argument of perigee: | 87.7342° |
| revolutions per day: | 14.82162786 |
| mean anomaly at epoch: | 272.4035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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