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 52138U 26145.10144683 +.00000000 +00000-0 +36631-4 0 00000
2 52138 53.2148 86.0938 0001436 74.9970 285.1181 15.08840340 07
| Epoch (UTC): | 25 May 2026 02:26:05 |
| Eccentricity: | 0.0001436 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 86.0938° |
| argument of perigee: | 74.9970° |
| revolutions per day: | 15.08840340 |
| mean anomaly at epoch: | 285.1181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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