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 49097U 26145.31492832 +.00000000 +00000-0 +82765-4 0 00004
2 49097 87.9157 10.4112 0002216 90.7276 269.4110 13.17648034 09
| Epoch (UTC): | 25 May 2026 07:33:29 |
| Eccentricity: | 0.0002216 |
| inclination: | 87.9157° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4112° |
| argument of perigee: | 90.7276° |
| revolutions per day: | 13.17648034 |
| mean anomaly at epoch: | 269.4110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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