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 61195U 26145.62706139 +.00000000 +00000-0 +12133-3 0 00000
2 61195 44.8565 237.3151 0005497 334.1031 25.9524 13.99139787 02
| Epoch (UTC): | 25 May 2026 15:02:58 |
| Eccentricity: | 0.0005497 |
| inclination: | 44.8565° |
| perigee height: | 893 km |
| apogee height: | 901 km |
| right ascension of ascending node: | 237.3151° |
| argument of perigee: | 334.1031° |
| revolutions per day: | 13.99139787 |
| mean anomaly at epoch: | 25.9524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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