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 30509U 26087.59738181 +.00000000 +00000-0 +13006-2 0 00007
2 30509 98.4622 317.9192 0100645 122.1919 268.3255 14.08382641 01
| Epoch (UTC): | 28 March 2026 14:20:13 |
| Eccentricity: | 0.0100645 |
| inclination: | 98.4622° |
| perigee height: | 792 km |
| apogee height: | 938 km |
| right ascension of ascending node: | 317.9192° |
| argument of perigee: | 122.1919° |
| revolutions per day: | 14.08382641 |
| mean anomaly at epoch: | 268.3255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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