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 13403U 26100.22707576 +.00000000 +00000-0 +19863-3 0 00009
2 13403 81.1465 155.8337 0025225 61.5169 298.8601 15.25214686 08
| Epoch (UTC): | 10 April 2026 05:26:59 |
| Eccentricity: | 0.0025225 |
| inclination: | 81.1465° |
| perigee height: | 473 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 155.8337° |
| argument of perigee: | 61.5169° |
| revolutions per day: | 15.25214686 |
| mean anomaly at epoch: | 298.8601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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