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 61749U 26145.60690508 +.00000000 +00000-0 +54058-3 0 00007
2 61749 97.3027 21.4132 0006419 16.6175 343.5288 15.53375395 05
| Epoch (UTC): | 25 May 2026 14:33:56 |
| Eccentricity: | 0.0006419 |
| inclination: | 97.3027° |
| perigee height: | 403 km |
| apogee height: | 411 km |
| right ascension of ascending node: | 21.4132° |
| argument of perigee: | 16.6175° |
| revolutions per day: | 15.53375395 |
| mean anomaly at epoch: | 343.5288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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