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 49101U 26145.33735948 +.00000000 +00000-0 +11389-2 0 00002
2 49101 87.8959 355.1883 0002182 88.5109 271.6269 13.12441878 02
| Epoch (UTC): | 25 May 2026 08:05:47 |
| Eccentricity: | 0.0002182 |
| inclination: | 87.8959° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1883° |
| argument of perigee: | 88.5109° |
| revolutions per day: | 13.12441878 |
| mean anomaly at epoch: | 271.6269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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