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 26072.92989797 +.00000000 +00000-0 +41194-4 0 00006
2 36095 67.1464 124.5656 0006218 244.2210 115.8233 13.97041304 09
| Epoch (UTC): | 13 March 2026 22:19:03 |
| Eccentricity: | 0.0006218 |
| inclination: | 67.1464° |
| perigee height: | 900 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 124.5656° |
| argument of perigee: | 244.2210° |
| revolutions per day: | 13.97041304 |
| mean anomaly at epoch: | 115.8233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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