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 52121U 26145.53937059 +.00000000 +00000-0 -76566-5 0 00009
2 52121 53.2135 84.1257 0001582 56.5680 303.5464 15.08837230 07
| Epoch (UTC): | 25 May 2026 12:56:41 |
| Eccentricity: | 0.0001582 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 84.1257° |
| argument of perigee: | 56.5680° |
| revolutions per day: | 15.08837230 |
| mean anomaly at epoch: | 303.5464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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