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 48404U 26145.25833652 +.00000000 +00000-0 +76127-4 0 00002
2 48404 53.1602 336.5506 0001413 67.5496 292.5655 15.31698812 01
| Epoch (UTC): | 25 May 2026 06:12:00 |
| Eccentricity: | 0.0001413 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 336.5506° |
| argument of perigee: | 67.5496° |
| revolutions per day: | 15.31698812 |
| mean anomaly at epoch: | 292.5655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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