▸Orbital parameters

Orbit class	SSO
Inclination	98.1209°
Eccentricity	0.0010966
Period	98.2 min
Apogee	682 km
Perigee	667 km
Mean motion	14.65861085 rev/day
RAAN	92.8173°
Arg of perigee	104.9405°
Mean anomaly	255.3013°
B*	5.2423e-5
Rev at epoch	17,334

▸Two-line element set (TLE)

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

1 56178U 23054A 26188.22290167 .00000238 00000-0 52423-4 0 9998

2 56178 98.1209 92.8173 0010966 104.9405 255.3013 14.65861085173344

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IMECE",
  "OBJECT_ID": "2023-054A",
  "EPOCH": "2026-07-07T05:20:58.704+00:00",
  "MEAN_MOTION": 14.65861085,
  "ECCENTRICITY": 0.0010966,
  "INCLINATION": 98.1209,
  "RA_OF_ASC_NODE": 92.8173,
  "ARG_OF_PERICENTER": 104.9405,
  "MEAN_ANOMALY": 255.3013,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 56178,
  "REV_AT_EPOCH": 17334,
  "BSTAR": 0.000052423,
  "MEAN_MOTION_DOT": 0.00000238,
  "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	IMECE
Operator	STRC Space Technologies Research InstituteHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Türkiye
Launch date	Apr 15, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	800HIGHvia 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/56178

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