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 39084U 26145.63838860 +.00000000 +00000-0 +69792-4 0 00004
2 39084 98.1837 216.0569 0001360 102.9102 257.2248 14.57119058 07
| Epoch (UTC): | 25 May 2026 15:19:16 |
| Eccentricity: | 0.0001360 |
| inclination: | 98.1837° |
| perigee height: | 702 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 216.0569° |
| argument of perigee: | 102.9102° |
| revolutions per day: | 14.57119058 |
| mean anomaly at epoch: | 257.2248° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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