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 61688U 26144.99124419 +.00000000 +00000-0 +12889-4 0 00000
2 61688 53.1609 10.4187 0000982 84.6046 275.5084 15.69708363 02
| Epoch (UTC): | 24 May 2026 23:47:23 |
| Eccentricity: | 0.0000982 |
| inclination: | 53.1609° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 10.4187° |
| argument of perigee: | 84.6046° |
| revolutions per day: | 15.69708363 |
| mean anomaly at epoch: | 275.5084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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