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 44528U 26145.62445580 +.00000000 +00000-0 +15025-3 0 00004
2 44528 98.3197 207.9070 0001577 141.9478 218.1820 14.35452749 07
| Epoch (UTC): | 25 May 2026 14:59:12 |
| Eccentricity: | 0.0001577 |
| inclination: | 98.3197° |
| perigee height: | 772 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 207.9070° |
| argument of perigee: | 141.9478° |
| revolutions per day: | 14.35452749 |
| mean anomaly at epoch: | 218.1820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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