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 61696U 26145.58869230 +.00000000 +00000-0 +14621-4 0 00008
2 61696 53.1596 7.0147 0000759 94.2029 265.9076 15.69710689 02
| Epoch (UTC): | 25 May 2026 14:07:43 |
| Eccentricity: | 0.0000759 |
| inclination: | 53.1596° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 7.0147° |
| argument of perigee: | 94.2029° |
| revolutions per day: | 15.69710689 |
| mean anomaly at epoch: | 265.9076° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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