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 53474U 26145.56594358 +.00000000 +00000-0 -38087-3 0 00009
2 53474 97.4479 265.5235 0001535 178.5126 181.6106 15.05677621 00
| Epoch (UTC): | 25 May 2026 13:34:57 |
| Eccentricity: | 0.0001535 |
| inclination: | 97.4479° |
| perigee height: | 548 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 265.5235° |
| argument of perigee: | 178.5126° |
| revolutions per day: | 15.05677621 |
| mean anomaly at epoch: | 181.6106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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