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 39295U 26086.77828007 +.00000000 +00000-0 +34054-2 0 00000
2 39295 100.4258 19.7011 0065320 16.8199 343.5078 13.48971256 05
| Epoch (UTC): | 27 March 2026 18:40:43 |
| Eccentricity: | 0.0065320 |
| inclination: | 100.4258° |
| perigee height: | 1027 km |
| apogee height: | 1125 km |
| right ascension of ascending node: | 19.7011° |
| argument of perigee: | 16.8199° |
| revolutions per day: | 13.48971256 |
| mean anomaly at epoch: | 343.5078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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