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 12474U 26150.40891580 +.00000000 +00000-0 +00000-0 0 00000
2 12474 10.9994 324.7984 0002552 304.0694 278.8531 0.98854351 06
| Epoch (UTC): | 30 May 2026 09:48:50 |
| Eccentricity: | 0.0002552 |
| inclination: | 10.9994° |
| perigee height: | 36178 km |
| apogee height: | 36200 km |
| right ascension of ascending node: | 324.7984° |
| argument of perigee: | 304.0694° |
| revolutions per day: | 0.98854351 |
| mean anomaly at epoch: | 278.8531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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