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 04320U 26133.50420354 +.00000000 +00000-0 +21760-4 0 00000
2 04320 101.3722 168.5141 0028176 22.4908 144.7451 12.52122043 00
| Epoch (UTC): | 13 May 2026 12:06:03 |
| Eccentricity: | 0.0028176 |
| inclination: | 101.3722° |
| perigee height: | 1434 km |
| apogee height: | 1478 km |
| right ascension of ascending node: | 168.5141° |
| argument of perigee: | 22.4908° |
| revolutions per day: | 12.52122043 |
| mean anomaly at epoch: | 144.7451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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