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 53154U 26145.51038584 +.00000000 +00000-0 +44554-4 0 00009
2 53154 53.2108 179.2583 0000986 62.0634 298.0458 15.08837320 01
| Epoch (UTC): | 25 May 2026 12:14:57 |
| Eccentricity: | 0.0000986 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 179.2583° |
| argument of perigee: | 62.0634° |
| revolutions per day: | 15.08837320 |
| mean anomaly at epoch: | 298.0458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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