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 48655U 26145.33001347 +.00000000 +00000-0 +39340-4 0 00003
2 48655 53.1582 117.5324 0001271 108.9648 251.1491 15.31706025 07
| Epoch (UTC): | 25 May 2026 07:55:13 |
| Eccentricity: | 0.0001271 |
| inclination: | 53.1582° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 117.5324° |
| argument of perigee: | 108.9648° |
| revolutions per day: | 15.31706025 |
| mean anomaly at epoch: | 251.1491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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