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 49083U 26145.53557153 +.00000000 +00000-0 -10061-2 0 00000
2 49083 87.8959 355.1634 0001485 91.6994 268.4305 13.12442638 07
| Epoch (UTC): | 25 May 2026 12:51:13 |
| Eccentricity: | 0.0001485 |
| inclination: | 87.8959° |
| perigee height: | 1213 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1634° |
| argument of perigee: | 91.6994° |
| revolutions per day: | 13.12442638 |
| mean anomaly at epoch: | 268.4305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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