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 26106.91869106 +.00000000 +00000-0 +12108-3 0 00004
2 13403 81.1452 147.9268 0024890 39.5780 320.7265 15.25251638 09
| Epoch (UTC): | 16 April 2026 22:02:54 |
| Eccentricity: | 0.0024890 |
| inclination: | 81.1452° |
| perigee height: | 473 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 147.9268° |
| argument of perigee: | 39.5780° |
| revolutions per day: | 15.25251638 |
| mean anomaly at epoch: | 320.7265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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