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 12635U 26150.14888412 +.00000000 +00000-0 +00000-0 0 00000
2 12635 13.9151 307.8806 0008623 168.4121 196.5932 0.98606843 02
| Epoch (UTC): | 30 May 2026 03:34:23 |
| Eccentricity: | 0.0008623 |
| inclination: | 13.9151° |
| perigee height: | 36223 km |
| apogee height: | 36297 km |
| right ascension of ascending node: | 307.8806° |
| argument of perigee: | 168.4121° |
| revolutions per day: | 0.98606843 |
| mean anomaly at epoch: | 196.5932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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