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 52470U 26145.21644588 +.00000000 +00000-0 -10903-4 0 00005
2 52470 53.2140 75.5754 0001565 80.2451 279.8717 15.08835653 00
| Epoch (UTC): | 25 May 2026 05:11:40 |
| Eccentricity: | 0.0001565 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 75.5754° |
| argument of perigee: | 80.2451° |
| revolutions per day: | 15.08835653 |
| mean anomaly at epoch: | 279.8717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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