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 52467U 26145.50349126 +.00000000 +00000-0 +37226-4 0 00009
2 52467 53.2138 74.2893 0001102 56.9215 303.1883 15.08832350 04
| Epoch (UTC): | 25 May 2026 12:05:01 |
| Eccentricity: | 0.0001102 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 74.2893° |
| argument of perigee: | 56.9215° |
| revolutions per day: | 15.08832350 |
| mean anomaly at epoch: | 303.1883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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