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 53628U 26145.54437625 +.00000000 +00000-0 +15954-4 0 00009
2 53628 53.2132 248.6686 0001083 87.1743 272.9373 15.08837911 00
| Epoch (UTC): | 25 May 2026 13:03:54 |
| Eccentricity: | 0.0001083 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 248.6686° |
| argument of perigee: | 87.1743° |
| revolutions per day: | 15.08837911 |
| mean anomaly at epoch: | 272.9373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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