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 26040.79214659 +.00000000 +00000-0 +64587-4 0 00004
2 12298 82.9521 143.5811 0030574 51.7663 65.0876 13.76929547 06
| Epoch (UTC): | 09 February 2026 19:00:41 |
| Eccentricity: | 0.0030574 |
| inclination: | 82.9521° |
| perigee height: | 952 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 143.5811° |
| argument of perigee: | 51.7663° |
| revolutions per day: | 13.76929547 |
| mean anomaly at epoch: | 65.0876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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