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 61787U 26145.58492750 +.00000000 +00000-0 +26819-3 0 00009
2 61787 97.3044 14.7326 0014401 35.1920 325.0272 15.36020133 06
| Epoch (UTC): | 25 May 2026 14:02:17 |
| Eccentricity: | 0.0014401 |
| inclination: | 97.3044° |
| perigee height: | 448 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 14.7326° |
| argument of perigee: | 35.1920° |
| revolutions per day: | 15.36020133 |
| mean anomaly at epoch: | 325.0272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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