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 26088.16106214 +.00000000 +00000-0 +46204-4 0 00009
2 32376 97.8878 272.9162 0001288 87.8197 272.3163 14.82148334 00
| Epoch (UTC): | 29 March 2026 03:51:55 |
| Eccentricity: | 0.0001288 |
| inclination: | 97.8878° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 272.9162° |
| argument of perigee: | 87.8197° |
| revolutions per day: | 14.82148334 |
| mean anomaly at epoch: | 272.3163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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