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 49441U 26145.50808766 +.00000000 +00000-0 +12003-4 0 00003
2 49441 53.2148 224.2668 0001128 86.6654 273.4467 15.08837738 07
| Epoch (UTC): | 25 May 2026 12:11:38 |
| Eccentricity: | 0.0001128 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 224.2668° |
| argument of perigee: | 86.6654° |
| revolutions per day: | 15.08837738 |
| mean anomaly at epoch: | 273.4467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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