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 47390U 26145.49069588 +.00000000 +00000-0 +97042-4 0 00009
2 47390 53.1601 69.1319 0001142 101.9467 258.1662 15.31708258 06
| Epoch (UTC): | 25 May 2026 11:46:36 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 69.1319° |
| argument of perigee: | 101.9467° |
| revolutions per day: | 15.31708258 |
| mean anomaly at epoch: | 258.1662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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