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 04321U 26068.62181221 +.00000000 +00000-0 +14712-4 0 00007
2 04321 101.3274 82.0270 0028035 97.7846 24.6707 12.52189375 07
| Epoch (UTC): | 09 March 2026 14:55:24 |
| Eccentricity: | 0.0028035 |
| inclination: | 101.3274° |
| perigee height: | 1433 km |
| apogee height: | 1477 km |
| right ascension of ascending node: | 82.0270° |
| argument of perigee: | 97.7846° |
| revolutions per day: | 12.52189375 |
| mean anomaly at epoch: | 24.6707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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