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 49447U 26145.39308552 +.00000000 +00000-0 +57083-4 0 00001
2 49447 53.2147 234.7833 0001048 90.3074 269.8038 15.08838492 02
| Epoch (UTC): | 25 May 2026 09:26:02 |
| Eccentricity: | 0.0001048 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 234.7833° |
| argument of perigee: | 90.3074° |
| revolutions per day: | 15.08838492 |
| mean anomaly at epoch: | 269.8038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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