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 48111U 26145.31063784 +.00000000 +00000-0 +11570-2 0 00004
2 48111 53.1557 156.3544 0006591 11.4802 348.6352 15.38808323 00
| Epoch (UTC): | 25 May 2026 07:27:19 |
| Eccentricity: | 0.0006591 |
| inclination: | 53.1557° |
| perigee height: | 445 km |
| apogee height: | 454 km |
| right ascension of ascending node: | 156.3544° |
| argument of perigee: | 11.4802° |
| revolutions per day: | 15.38808323 |
| mean anomaly at epoch: | 348.6352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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