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 52444U 26145.56818494 +.00000000 +00000-0 +76050-3 0 00006
2 52444 97.5685 257.5518 0004707 135.8336 224.3302 15.70108234 08
| Epoch (UTC): | 25 May 2026 13:38:11 |
| Eccentricity: | 0.0004707 |
| inclination: | 97.5685° |
| perigee height: | 355 km |
| apogee height: | 362 km |
| right ascension of ascending node: | 257.5518° |
| argument of perigee: | 135.8336° |
| revolutions per day: | 15.70108234 |
| mean anomaly at epoch: | 224.3302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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