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 48099U 26145.46944808 +.00000000 +00000-0 +97950-4 0 00008
2 48099 53.1585 170.6852 0001257 92.5655 267.5490 15.31691391 07
| Epoch (UTC): | 25 May 2026 11:16:00 |
| Eccentricity: | 0.0001257 |
| inclination: | 53.1585° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 170.6852° |
| argument of perigee: | 92.5655° |
| revolutions per day: | 15.31691391 |
| mean anomaly at epoch: | 267.5490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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