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 47896U 26145.10087332 +.00000000 +00000-0 +27534-4 0 00004
2 47896 53.1583 285.5719 0001118 87.3474 272.7656 15.31705154 09
| Epoch (UTC): | 25 May 2026 02:25:15 |
| Eccentricity: | 0.0001118 |
| inclination: | 53.1583° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 285.5719° |
| argument of perigee: | 87.3474° |
| revolutions per day: | 15.31705154 |
| mean anomaly at epoch: | 272.7656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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