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 36834U 26145.66320887 +.00000000 +00000-0 +22450-3 0 00001
2 36834 97.8994 169.2477 0001626 91.6517 48.3835 14.85270259 06
| Epoch (UTC): | 25 May 2026 15:55:01 |
| Eccentricity: | 0.0001626 |
| inclination: | 97.8994° |
| perigee height: | 612 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 169.2477° |
| argument of perigee: | 91.6517° |
| revolutions per day: | 14.85270259 |
| mean anomaly at epoch: | 48.3835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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