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 48694U 26145.24199381 +.00000000 +00000-0 +10549-4 0 00002
2 48694 53.1593 82.4359 0001227 84.9735 275.1407 15.31703309 06
| Epoch (UTC): | 25 May 2026 05:48:28 |
| Eccentricity: | 0.0001227 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 82.4359° |
| argument of perigee: | 84.9735° |
| revolutions per day: | 15.31703309 |
| mean anomaly at epoch: | 275.1407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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