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 58048U 26145.49171839 +.00000000 +00000-0 +22817-4 0 00002
2 58048 53.1596 171.3001 0001124 78.3702 281.7425 15.30195874 06
| Epoch (UTC): | 25 May 2026 11:48:04 |
| Eccentricity: | 0.0001124 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.3001° |
| argument of perigee: | 78.3702° |
| revolutions per day: | 15.30195874 |
| mean anomaly at epoch: | 281.7425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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