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 61518U 26145.27693932 +.00000000 +00000-0 +19879-4 0 00001
2 61518 53.1603 146.3236 0001192 81.7367 278.3770 15.31702078 09
| Epoch (UTC): | 25 May 2026 06:38:47 |
| Eccentricity: | 0.0001192 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 146.3236° |
| argument of perigee: | 81.7367° |
| revolutions per day: | 15.31702078 |
| mean anomaly at epoch: | 278.3770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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