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 48440U 26145.62098176 +.00000000 +00000-0 +42675-5 0 00009
2 48440 53.1583 180.3066 0000988 88.0281 272.0833 15.31693584 03
| Epoch (UTC): | 25 May 2026 14:54:12 |
| Eccentricity: | 0.0000988 |
| inclination: | 53.1583° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 180.3066° |
| argument of perigee: | 88.0281° |
| revolutions per day: | 15.31693584 |
| mean anomaly at epoch: | 272.0833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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