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 52488U 26145.51820713 +.00000000 +00000-0 +18369-4 0 00006
2 52488 53.2129 74.2229 0001283 88.0460 272.0680 15.08844357 07
| Epoch (UTC): | 25 May 2026 12:26:13 |
| Eccentricity: | 0.0001283 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 74.2229° |
| argument of perigee: | 88.0460° |
| revolutions per day: | 15.08844357 |
| mean anomaly at epoch: | 272.0680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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