▸Orbital parameters

Orbit class	GEO
Inclination	3.3357°
Eccentricity	0.0003838
Period	1436.1 min
Apogee	35,803 km
Perigee	35,771 km
Mean motion	1.00271637 rev/day
RAAN	79.1831°
Arg of perigee	25.3710°
Mean anomaly	113.7106°
B*	0.0000e+0
Rev at epoch	4,146

▸Two-line element set (TLE)

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

1 28378U 04027A 26188.12303007 -.00000037 00000-0 00000-0 0 9993

2 28378 3.3357 79.1831 0003838 25.3710 113.7106 1.00271637 41461

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ANIK F2",
  "OBJECT_ID": "2004-027A",
  "EPOCH": "2026-07-07T02:57:09.798+00:00",
  "MEAN_MOTION": 1.00271637,
  "ECCENTRICITY": 0.0003838,
  "INCLINATION": 3.3357,
  "RA_OF_ASC_NODE": 79.1831,
  "ARG_OF_PERICENTER": 25.371,
  "MEAN_ANOMALY": 113.7106,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 28378,
  "REV_AT_EPOCH": 4146,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -3.7e-7,
  "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	ANIK F2
Operator	Telesat CanadaHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Canada
Launch date	Jul 18, 2004HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5965HIGHvia 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/28378

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