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 26040.26582155 +.00000000 +00000-0 +68319-4 0 00002
2 12298 82.9520 143.9717 0030584 53.1737 336.1888 13.76929477 00
| Epoch (UTC): | 09 February 2026 06:22:46 |
| Eccentricity: | 0.0030584 |
| inclination: | 82.9520° |
| perigee height: | 952 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 143.9717° |
| argument of perigee: | 53.1737° |
| revolutions per day: | 13.76929477 |
| mean anomaly at epoch: | 336.1888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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