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 48361U 26145.32036601 +.00000000 +00000-0 +90366-4 0 00002
2 48361 53.1620 1.7336 0001201 93.1096 267.0043 15.31698008 06
| Epoch (UTC): | 25 May 2026 07:41:19 |
| Eccentricity: | 0.0001201 |
| inclination: | 53.1620° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 1.7336° |
| argument of perigee: | 93.1096° |
| revolutions per day: | 15.31698008 |
| mean anomaly at epoch: | 267.0043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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