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 49460U 26145.62124811 +.00000000 +00000-0 -36706-4 0 00006
2 49460 53.2136 233.7616 0001147 94.3704 265.7420 15.08842831 09
| Epoch (UTC): | 25 May 2026 14:54:35 |
| Eccentricity: | 0.0001147 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 233.7616° |
| argument of perigee: | 94.3704° |
| revolutions per day: | 15.08842831 |
| mean anomaly at epoch: | 265.7420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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