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 26041.88484602 +.00000000 +00000-0 +54191-4 0 00002
2 12298 82.9520 142.7701 0030520 48.8050 81.4426 13.76929659 09
| Epoch (UTC): | 10 February 2026 21:14:10 |
| Eccentricity: | 0.0030520 |
| inclination: | 82.9520° |
| perigee height: | 952 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 142.7701° |
| argument of perigee: | 48.8050° |
| revolutions per day: | 13.76929659 |
| mean anomaly at epoch: | 81.4426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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