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 42838U 26145.48656788 +.00000000 +00000-0 +63868-3 0 00002
2 42838 97.3684 326.3402 0009914 89.7020 270.5359 15.33803298 06
| Epoch (UTC): | 25 May 2026 11:40:39 |
| Eccentricity: | 0.0009914 |
| inclination: | 97.3684° |
| perigee height: | 458 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 326.3402° |
| argument of perigee: | 89.7020° |
| revolutions per day: | 15.33803298 |
| mean anomaly at epoch: | 270.5359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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