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 26038.85259203 +.00000000 +00000-0 +48473-4 0 00009
2 36095 67.1461 207.4368 0007280 248.0583 111.9728 13.97037249 01
| Epoch (UTC): | 07 February 2026 20:27:43 |
| Eccentricity: | 0.0007280 |
| inclination: | 67.1461° |
| perigee height: | 899 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 207.4368° |
| argument of perigee: | 248.0583° |
| revolutions per day: | 13.97037249 |
| mean anomaly at epoch: | 111.9728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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