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 48435U 26145.52902391 +.00000000 +00000-0 +45819-4 0 00007
2 48435 53.1600 167.8844 0001248 80.1310 279.9833 15.31704202 03
| Epoch (UTC): | 25 May 2026 12:41:47 |
| Eccentricity: | 0.0001248 |
| inclination: | 53.1600° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 167.8844° |
| argument of perigee: | 80.1310° |
| revolutions per day: | 15.31704202 |
| mean anomaly at epoch: | 279.9833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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