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 51841U 26145.02078443 +.00000000 +00000-0 +10413-2 0 00009
2 51841 97.3581 241.6153 0007775 226.5467 133.5166 16.01791082 04
| Epoch (UTC): | 25 May 2026 00:29:55 |
| Eccentricity: | 0.0007775 |
| inclination: | 97.3581° |
| perigee height: | 264 km |
| apogee height: | 275 km |
| right ascension of ascending node: | 241.6153° |
| argument of perigee: | 226.5467° |
| revolutions per day: | 16.01791082 |
| mean anomaly at epoch: | 133.5166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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