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 26037.63554361 +.00000000 +00000-0 +33252-4 0 00006
2 36095 67.1459 210.3966 0007347 248.3768 111.6534 13.97036984 04
| Epoch (UTC): | 06 February 2026 15:15:10 |
| Eccentricity: | 0.0007347 |
| inclination: | 67.1459° |
| perigee height: | 899 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 210.3966° |
| argument of perigee: | 248.3768° |
| revolutions per day: | 13.97036984 |
| mean anomaly at epoch: | 111.6534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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