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 53542U 26145.20312380 +.00000000 +00000-0 -85485-4 0 00004
2 53542 53.2135 80.6373 0001390 101.4646 258.6503 15.08828940 06
| Epoch (UTC): | 25 May 2026 04:52:29 |
| Eccentricity: | 0.0001390 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 80.6373° |
| argument of perigee: | 101.4646° |
| revolutions per day: | 15.08828940 |
| mean anomaly at epoch: | 258.6503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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