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 52984U 26142.29965627 +.00000000 +00000-0 +00000-0 0 00002
2 52984 64.3148 315.3974 0010092 278.3503 81.5318 2.13101899 08
| Epoch (UTC): | 22 May 2026 07:11:30 |
| Eccentricity: | 0.0010092 |
| inclination: | 64.3148° |
| perigee height: | 19104 km |
| apogee height: | 19156 km |
| right ascension of ascending node: | 315.3974° |
| argument of perigee: | 278.3503° |
| revolutions per day: | 2.13101899 |
| mean anomaly at epoch: | 81.5318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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