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 49099U 26145.56285438 +.00000000 +00000-0 -71033-4 0 00002
2 49099 87.9151 10.3794 0001916 86.7403 273.3948 13.17650667 01
| Epoch (UTC): | 25 May 2026 13:30:30 |
| Eccentricity: | 0.0001916 |
| inclination: | 87.9151° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3794° |
| argument of perigee: | 86.7403° |
| revolutions per day: | 13.17650667 |
| mean anomaly at epoch: | 273.3948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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