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 26096.83839395 +.00000000 +00000-0 +18702-3 0 00008
2 39416 97.7645 51.1216 0037536 87.9156 272.6360 14.91387970 04
| Epoch (UTC): | 06 April 2026 20:07:17 |
| Eccentricity: | 0.0037536 |
| inclination: | 97.7645° |
| perigee height: | 567 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 51.1216° |
| argument of perigee: | 87.9156° |
| revolutions per day: | 14.91387970 |
| mean anomaly at epoch: | 272.6360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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