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 61699U 26145.00095034 +.00000000 +00000-0 +15261-4 0 00002
2 61699 53.1596 9.7412 0000947 120.4197 239.6915 15.69710426 05
| Epoch (UTC): | 25 May 2026 00:01:22 |
| Eccentricity: | 0.0000947 |
| inclination: | 53.1596° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 9.7412° |
| argument of perigee: | 120.4197° |
| revolutions per day: | 15.69710426 |
| mean anomaly at epoch: | 239.6915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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