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 12458U 26053.65294264 +.00000000 +00000-0 +57336-4 0 00005
2 12458 89.8439 90.3430 0012314 264.8228 217.1226 13.23286067 04
| Epoch (UTC): | 22 February 2026 15:40:14 |
| Eccentricity: | 0.0012314 |
| inclination: | 89.8439° |
| perigee height: | 1163 km |
| apogee height: | 1181 km |
| right ascension of ascending node: | 90.3430° |
| argument of perigee: | 264.8228° |
| revolutions per day: | 13.23286067 |
| mean anomaly at epoch: | 217.1226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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