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 05395U 26088.18683641 +.00000000 +00000-0 +31893-3 0 00003
2 05395 87.6228 340.2908 0053121 312.3204 47.3503 14.42284213 03
| Epoch (UTC): | 29 March 2026 04:29:02 |
| Eccentricity: | 0.0053121 |
| inclination: | 87.6228° |
| perigee height: | 713 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 340.2908° |
| argument of perigee: | 312.3204° |
| revolutions per day: | 14.42284213 |
| mean anomaly at epoch: | 47.3503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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