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 49417U 26145.50712558 +.00000000 +00000-0 +44897-4 0 00005
2 49417 53.2147 233.9254 0001107 84.4620 275.6499 15.08838704 06
| Epoch (UTC): | 25 May 2026 12:10:15 |
| Eccentricity: | 0.0001107 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 233.9254° |
| argument of perigee: | 84.4620° |
| revolutions per day: | 15.08838704 |
| mean anomaly at epoch: | 275.6499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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