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 00340U 26152.51907644 +.00000000 +00000-0 -42310-3 0 00006
2 00340 44.8053 349.2074 2427186 111.0542 298.5945 9.12893189 08
| Epoch (UTC): | 01 June 2026 12:27:28 |
| Eccentricity: | 0.2427186 |
| inclination: | 44.8053° |
| perigee height: | 945 km |
| apogee height: | 5640 km |
| right ascension of ascending node: | 349.2074° |
| argument of perigee: | 111.0542° |
| revolutions per day: | 9.12893189 |
| mean anomaly at epoch: | 298.5945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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