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 36095U 26044.79465013 +.00000000 +00000-0 +27913-4 0 00003
2 36095 67.1470 192.9858 0007086 247.1825 112.8512 13.97037910 02
| Epoch (UTC): | 13 February 2026 19:04:17 |
| Eccentricity: | 0.0007086 |
| inclination: | 67.1470° |
| perigee height: | 899 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 192.9858° |
| argument of perigee: | 247.1825° |
| revolutions per day: | 13.97037910 |
| mean anomaly at epoch: | 112.8512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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