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 26108.88678354 +.00000000 +00000-0 +13586-3 0 00006
2 13403 81.1448 145.6008 0024756 33.1652 327.1127 15.25263498 05
| Epoch (UTC): | 18 April 2026 21:16:58 |
| Eccentricity: | 0.0024756 |
| inclination: | 81.1448° |
| perigee height: | 473 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 145.6008° |
| argument of perigee: | 33.1652° |
| revolutions per day: | 15.25263498 |
| mean anomaly at epoch: | 327.1127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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