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 30325U 26087.49301568 +.00000000 +00000-0 +13437-3 0 00006
2 30325 98.7258 108.5605 0015388 318.2096 41.7898 14.09144525 05
| Epoch (UTC): | 28 March 2026 11:49:56 |
| Eccentricity: | 0.0015388 |
| inclination: | 98.7258° |
| perigee height: | 851 km |
| apogee height: | 873 km |
| right ascension of ascending node: | 108.5605° |
| argument of perigee: | 318.2096° |
| revolutions per day: | 14.09144525 |
| mean anomaly at epoch: | 41.7898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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