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 49096U 26145.13574714 +.00000000 +00000-0 -51564-3 0 00006
2 49096 87.8951 355.2662 0001752 86.2065 273.9264 13.12441333 07
| Epoch (UTC): | 25 May 2026 03:15:28 |
| Eccentricity: | 0.0001752 |
| inclination: | 87.8951° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2662° |
| argument of perigee: | 86.2065° |
| revolutions per day: | 13.12441333 |
| mean anomaly at epoch: | 273.9264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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