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 48270U 26145.12513933 +.00000000 +00000-0 +22842-3 0 00000
2 48270 97.5623 200.5644 0005504 1.5248 358.5993 15.03261346 03
| Epoch (UTC): | 25 May 2026 03:00:12 |
| Eccentricity: | 0.0005504 |
| inclination: | 97.5623° |
| perigee height: | 553 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 200.5644° |
| argument of perigee: | 1.5248° |
| revolutions per day: | 15.03261346 |
| mean anomaly at epoch: | 358.5993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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