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 12298U 26044.72356169 +.00000000 +00000-0 +46617-4 0 00008
2 12298 82.9518 140.6634 0030396 41.1177 112.5465 13.76929930 06
| Epoch (UTC): | 13 February 2026 17:21:55 |
| Eccentricity: | 0.0030396 |
| inclination: | 82.9518° |
| perigee height: | 952 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 140.6634° |
| argument of perigee: | 41.1177° |
| revolutions per day: | 13.76929930 |
| mean anomaly at epoch: | 112.5465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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