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 26106.18073965 +.00000000 +00000-0 +74889-4 0 00007
2 12458 89.8432 89.5486 0015988 117.3466 253.7127 13.23292208 04
| Epoch (UTC): | 16 April 2026 04:20:15 |
| Eccentricity: | 0.0015988 |
| inclination: | 89.8432° |
| perigee height: | 1160 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 89.5486° |
| argument of perigee: | 117.3466° |
| revolutions per day: | 13.23292208 |
| mean anomaly at epoch: | 253.7127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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