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 53947U 26145.36932581 +.00000000 +00000-0 +58628-3 0 00008
2 53947 35.0047 24.8403 0005401 297.2091 62.8077 15.36783323 01
| Epoch (UTC): | 25 May 2026 08:51:49 |
| Eccentricity: | 0.0005401 |
| inclination: | 35.0047° |
| perigee height: | 452 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 24.8403° |
| argument of perigee: | 297.2091° |
| revolutions per day: | 15.36783323 |
| mean anomaly at epoch: | 62.8077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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