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 15945U 26109.13478156 +.00000000 +00000-0 +31903-4 0 00000
2 15945 82.5285 346.9118 0020164 60.7845 299.5385 14.86472943 00
| Epoch (UTC): | 19 April 2026 03:14:05 |
| Eccentricity: | 0.0020164 |
| inclination: | 82.5285° |
| perigee height: | 595 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 346.9118° |
| argument of perigee: | 60.7845° |
| revolutions per day: | 14.86472943 |
| mean anomaly at epoch: | 299.5385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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