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 59380U 26145.32362145 +.00000000 +00000-0 +19944-4 0 00003
2 59380 53.1604 261.8947 0001213 85.6630 274.4512 15.34388494 02
| Epoch (UTC): | 25 May 2026 07:46:00 |
| Eccentricity: | 0.0001213 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 261.8947° |
| argument of perigee: | 85.6630° |
| revolutions per day: | 15.34388494 |
| mean anomaly at epoch: | 274.4512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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