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 39416U 26145.61292455 +.00000000 +00000-0 +12578-3 0 00004
2 39416 97.7696 99.1600 0034343 287.0817 72.6641 14.91505059 09
| Epoch (UTC): | 25 May 2026 14:42:36 |
| Eccentricity: | 0.0034343 |
| inclination: | 97.7696° |
| perigee height: | 569 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 99.1600° |
| argument of perigee: | 287.0817° |
| revolutions per day: | 14.91505059 |
| mean anomaly at epoch: | 72.6641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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