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 26088.09805544 +.00000000 +00000-0 +11219-3 0 00008
2 04320 101.3800 125.0836 0028661 110.0651 311.4311 12.52121025 01
| Epoch (UTC): | 29 March 2026 02:21:11 |
| Eccentricity: | 0.0028661 |
| inclination: | 101.3800° |
| perigee height: | 1433 km |
| apogee height: | 1478 km |
| right ascension of ascending node: | 125.0836° |
| argument of perigee: | 110.0651° |
| revolutions per day: | 12.52121025 |
| mean anomaly at epoch: | 311.4311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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