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 49297U 26145.21737775 +.00000000 +00000-0 -98682-4 0 00009
2 49297 87.9154 309.5446 0001689 94.6446 265.4880 13.19726368 04
| Epoch (UTC): | 25 May 2026 05:13:01 |
| Eccentricity: | 0.0001689 |
| inclination: | 87.9154° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5446° |
| argument of perigee: | 94.6446° |
| revolutions per day: | 13.19726368 |
| mean anomaly at epoch: | 265.4880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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