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 39155U 26144.91627111 +.00000000 +00000-0 +00000-0 0 00001
2 39155 65.4077 74.3848 0023600 236.0366 123.7299 2.13103066 00
| Epoch (UTC): | 24 May 2026 21:59:25 |
| Eccentricity: | 0.0023600 |
| inclination: | 65.4077° |
| perigee height: | 19070 km |
| apogee height: | 19190 km |
| right ascension of ascending node: | 74.3848° |
| argument of perigee: | 236.0366° |
| revolutions per day: | 2.13103066 |
| mean anomaly at epoch: | 123.7299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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