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 48573U 26145.66668980 +.00000000 +00000-0 -23646-3 0 00002
2 48573 53.1586 129.3409 0001456 87.9093 312.4044 15.31721905 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001456 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 129.3409° |
| argument of perigee: | 87.9093° |
| revolutions per day: | 15.31721905 |
| mean anomaly at epoch: | 312.4044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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