▸Orbital parameters

Orbit class	SSO
Inclination	97.4024°
Eccentricity	0.0003712
Period	94.7 min
Apogee	506 km
Perigee	501 km
Mean motion	15.20818674 rev/day
RAAN	85.5141°
Arg of perigee	349.4997°
Mean anomaly	10.6160°
B*	1.4900e-4
Rev at epoch	982

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 69011U 26100AH 26188.02348441 .00003218 00000-0 14900-3 0 9998

2 69011 97.4024 85.5141 0003712 349.4997 10.6160 15.20818674 9822

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EYCORE-1",
  "OBJECT_ID": "2026-100AH",
  "EPOCH": "2026-07-07T00:33:49.053+00:00",
  "MEAN_MOTION": 15.20818674,
  "ECCENTRICITY": 0.0003712,
  "INCLINATION": 97.4024,
  "RA_OF_ASC_NODE": 85.5141,
  "ARG_OF_PERICENTER": 349.4997,
  "MEAN_ANOMALY": 10.616,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69011,
  "REV_AT_EPOCH": 982,
  "BSTAR": 0.000149,
  "MEAN_MOTION_DOT": 0.00003218,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	EYCORE-1
Operator	Eycore Sp z.o.o.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Poland
Launch date	May 3, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	200HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/69011

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.