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 53702U 26144.98367628 +.00000000 +00000-0 -87974-4 0 00006
2 53702 53.2129 246.5240 0001116 90.7843 269.3277 15.08842154 08
| Epoch (UTC): | 24 May 2026 23:36:29 |
| Eccentricity: | 0.0001116 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 246.5240° |
| argument of perigee: | 90.7843° |
| revolutions per day: | 15.08842154 |
| mean anomaly at epoch: | 269.3277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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