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 48317U 26145.54757973 +.00000000 +00000-0 +73579-4 0 00006
2 48317 53.1585 90.7084 0001104 96.3972 263.7155 15.31711987 04
| Epoch (UTC): | 25 May 2026 13:08:30 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.1585° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 90.7084° |
| argument of perigee: | 96.3972° |
| revolutions per day: | 15.31711987 |
| mean anomaly at epoch: | 263.7155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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