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 48459U 26145.49979890 +.00000000 +00000-0 +10833-4 0 00005
2 48459 53.1587 180.9115 0001076 91.5380 268.5745 15.31705822 07
| Epoch (UTC): | 25 May 2026 11:59:42 |
| Eccentricity: | 0.0001076 |
| inclination: | 53.1587° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 180.9115° |
| argument of perigee: | 91.5380° |
| revolutions per day: | 15.31705822 |
| mean anomaly at epoch: | 268.5745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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