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 53033U 26145.13228522 +.00000000 +00000-0 -13042-3 0 00004
2 53033 53.2126 90.9565 0002261 88.4068 271.7183 15.08833808 07
| Epoch (UTC): | 25 May 2026 03:10:29 |
| Eccentricity: | 0.0002261 |
| inclination: | 53.2126° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 90.9565° |
| argument of perigee: | 88.4068° |
| revolutions per day: | 15.08833808 |
| mean anomaly at epoch: | 271.7183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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