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 48471U 26145.41897507 +.00000000 +00000-0 +43373-3 0 00009
2 48471 53.1577 194.1737 0000990 93.3202 266.7913 15.31716520 08
| Epoch (UTC): | 25 May 2026 10:03:19 |
| Eccentricity: | 0.0000990 |
| inclination: | 53.1577° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 194.1737° |
| argument of perigee: | 93.3202° |
| revolutions per day: | 15.31716520 |
| mean anomaly at epoch: | 266.7913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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