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 12783U 26087.89245250 +.00000000 +00000-0 +42569-4 0 00002
2 12783 65.1155 289.7450 0045532 219.3999 140.3749 13.85533777 09
| Epoch (UTC): | 28 March 2026 21:25:07 |
| Eccentricity: | 0.0045532 |
| inclination: | 65.1155° |
| perigee height: | 911 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 289.7450° |
| argument of perigee: | 219.3999° |
| revolutions per day: | 13.85533777 |
| mean anomaly at epoch: | 140.3749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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